Knowledge

Two-body problem

Source 📝

762: 110: 4061: 3753: 3518: 705: 2104: 45: 36: 556:", treats one object as the immobile source of a force acting on the other. One then seeks to predict the motion of the single remaining mobile object. Such an approximation can give useful results when one object is much more massive than the other (as with a light planet orbiting a heavy star, where the star can be treated as essentially stationary). 3264: 1900: 4056:{\displaystyle {\begin{aligned}E_{1}&={\frac {\mu }{m_{1}}}E={\frac {1}{2}}m_{1}{\dot {\mathbf {x} }}_{1}^{2}+{\frac {\mu }{m_{1}}}U(\mathbf {r} )\\E_{2}&={\frac {\mu }{m_{2}}}E={\frac {1}{2}}m_{2}{\dot {\mathbf {x} }}_{2}^{2}+{\frac {\mu }{m_{2}}}U(\mathbf {r} )\\E_{\text{tot}}&=E_{1}+E_{2}\end{aligned}}} 3037: 632:
being the obvious physical example. In practice, such problems rarely arise. Except perhaps in experimental apparatus or other specialized equipment, we rarely encounter electrostatically interacting objects which are moving fast enough, and in such a direction, as to avoid colliding, and/or which
594:
The two-body problem is interesting in astronomy because pairs of astronomical objects are often moving rapidly in arbitrary directions (so their motions become interesting), widely separated from one another (so they will not collide) and even more widely separated from other objects (so outside
1608: 1760: 2265: 852: 2867: 3513:{\displaystyle E_{\text{tot}}={\frac {1}{2}}m_{1}{\dot {\mathbf {x} }}_{1}^{2}+{\frac {1}{2}}m_{2}{\dot {\mathbf {x} }}_{2}^{2}+U(\mathbf {r} )={\frac {1}{2}}(m_{1}+m_{2}){\dot {\mathbf {R} }}^{2}+{1 \over 2}\mu {\dot {\mathbf {r} }}^{2}+U(\mathbf {r} )} 2416: 2924: 2099:{\displaystyle {\ddot {\mathbf {r} }}={\ddot {\mathbf {x} }}_{1}-{\ddot {\mathbf {x} }}_{2}=\left({\frac {\mathbf {F} _{12}}{m_{1}}}-{\frac {\mathbf {F} _{21}}{m_{2}}}\right)=\left({\frac {1}{m_{1}}}+{\frac {1}{m_{2}}}\right)\mathbf {F} _{12}} 1299: 1185: 1449: 3144: 2749: 2639: 602:, each member of a pair of such objects will orbit their mutual center of mass in an elliptical pattern, unless they are moving fast enough to escape one another entirely, in which case their paths will diverge along other planar 3598: 904: 1632: 4253: 678:
are necessary for any useful understanding of the electron's real behavior. Solving the classical two-body problem for an electron orbiting an atomic nucleus is misleading and does not produce many useful insights.
4151: 3726: 3670: 3758: 2169: 606:. If one object is very much heavier than the other, it will move far less than the other with reference to the shared center of mass. The mutual center of mass may even be inside the larger object. 2795: 2295: 1844: 1208: 1094: 2495: 2462: 559:
However, the one-body approximation is usually unnecessary except as a stepping stone. For many forces, including gravitational ones, the general version of the two-body problem can be
1799: 771: 3074: 2643: 2533: 754:
The complete two-body problem can be solved by re-formulating it as two one-body problems: a trivial one and one that involves solving for the motion of one particle in an external
953: 1436: 648:
Although the two-body model treats the objects as point particles, classical mechanics only apply to systems of macroscopic scale. Most behavior of subatomic particles
3529: 2285: 4187: 3032:{\displaystyle \mathbf {N} ={\frac {d\mathbf {L} }{dt}}={\dot {\mathbf {r} }}\times \mu {\dot {\mathbf {r} }}+\mathbf {r} \times \mu {\ddot {\mathbf {r} }}\ ,} 720: 688: 4094: 3674: 1603:{\displaystyle m_{1}{\ddot {\mathbf {x} }}_{1}+m_{2}{\ddot {\mathbf {x} }}_{2}=(m_{1}+m_{2}){\ddot {\mathbf {R} }}=\mathbf {F} _{12}+\mathbf {F} _{21}=0} 3621: 1380:
between the masses changes with time. The solutions of these independent one-body problems can be combined to obtain the solutions for the trajectories
620:
In principle, the same solutions apply to macroscopic problems involving objects interacting not only through gravity, but through any other attractive
857: 526:
is to calculate and predict the motion of two massive bodies that are orbiting each other in space. The problem assumes that the two bodies are
1897:
Dividing both force equations by the respective masses, subtracting the second equation from the first, and rearranging gives the equation
549:. A two-point-particle model of such a system nearly always describes its behavior well enough to provide useful insights and predictions. 530:
that interact only with one another; the only force affecting each object arises from the other one, and all other objects are ignored.
1755:{\displaystyle {\ddot {\mathbf {R} }}\equiv {\frac {m_{1}{\ddot {\mathbf {x} }}_{1}+m_{2}{\ddot {\mathbf {x} }}_{2}}{m_{1}+m_{2}}}.} 77:
Two bodies with a "slight" difference in mass orbiting a common barycenter. Their sizes and this type of orbit are similar to the
505: 1083: 20: 1767: 277: 2260:{\displaystyle \mu {\ddot {\mathbf {r} }}=\mathbf {F} _{12}(\mathbf {x} _{1},\mathbf {x} _{2})=\mathbf {F} (\mathbf {r} )} 1338:
Adding and subtracting these two equations decouples them into two one-body problems, which can be solved independently.
346: 2431:
is the key to the two-body problem. The solution depends on the specific force between the bodies, which is defined by
2166:, and the laws of physics would have to change from place to place. The subtracted equation can therefore be written: 2138:
The force between the two objects, which originates in the two objects, should only be a function of their separation
4454: 4426: 4383: 3189: 1804: 4441: 4071: 847:{\displaystyle {\boldsymbol {R}}={\frac {m_{1}}{M}}{\boldsymbol {x}}_{1}+{\frac {m_{2}}{M}}{\boldsymbol {x}}_{2}} 610: 553: 2862:{\displaystyle \mathbf {L} =\mathbf {r} \times \mathbf {p} =\mathbf {r} \times \mu {\frac {d\mathbf {r} }{dt}},} 2467: 2434: 167: 4282: 758:. Since many one-body problems can be solved exactly, the corresponding two-body problem can also be solved. 2411:{\displaystyle \mu ={\frac {1}{{\frac {1}{m_{1}}}+{\frac {1}{m_{2}}}}}={\frac {m_{1}m_{2}}{m_{1}+m_{2}}}.} 498: 431: 4494: 3171: 1611: 637: 1335:
position vectors denote their second derivative with respect to time, or their acceleration vectors.
909: 24: 19:
This article is about the two-body problem in classical mechanics. For the relativistic version, see
3174:) that the force between two particles acts along the line between their positions, it follows that 1294:{\displaystyle \mathbf {F} _{21}(\mathbf {x} _{1},\mathbf {x} _{2})=m_{2}{\ddot {\mathbf {x} }}_{2}} 1180:{\displaystyle \mathbf {F} _{12}(\mathbf {x} _{1},\mathbf {x} _{2})=m_{1}{\ddot {\mathbf {x} }}_{1}} 652:
be predicted under the classical assumptions underlying this article or using the mathematics here.
1875: 563:, allowing it to be solved completely, and giving a solution simple enough to be used effectively. 426: 341: 3523: 1419: 730: 533:
The most prominent example of the classical two-body problem is the gravitational case (see also
297: 1889:
of the center of mass can be determined at all times from the initial positions and velocities.
4470: 4277: 3139:{\displaystyle \mathbf {N} \ =\ {\frac {d\mathbf {L} }{dt}}=\mathbf {r} \times \mathbf {F} \ ,} 2744:{\displaystyle \mathbf {x} _{2}(t)=\mathbf {R} (t)-{\frac {m_{1}}{m_{1}+m_{2}}}\mathbf {r} (t)} 2634:{\displaystyle \mathbf {x} _{1}(t)=\mathbf {R} (t)+{\frac {m_{2}}{m_{1}+m_{2}}}\mathbf {r} (t)} 2163: 491: 214: 2132: 2107: 726: 537:), arising in astronomy for predicting the orbits (or escapes from orbit) of objects such as 399: 234: 142: 4342: 3040: 2768: 272: 229: 219: 147: 2270: 636:
The dynamical system of a two-body system under the influence of torque turns out to be a
8: 519: 314: 152: 4346: 4372: 4305: 3240: 2901:(with these written taking the center of mass as the origin, and thus both parallel to 2498: 1331:
is the force on mass 2 due to its interactions with mass 1. The two dots on top of the
765: 625: 581: ≥ 3) cannot be solved in terms of first integrals, except in special cases. 567: 387: 262: 4450: 4436: 4422: 4379: 3258: 675: 302: 239: 118: 1360:
equation (2) from equation (1) results in an equation that describes how the vector
4350: 3244: 2784: 2767:
The motion of two bodies with respect to each other always lies in a plane (in the
629: 621: 472: 421: 130: 4489: 4406: 2775: 734: 714: 689:
Classical central-force problem § Relation to the classical two-body problem
477: 382: 292: 267: 674:"). However, electrons don't actually orbit nuclei in any meaningful sense, and 4446: 4418: 4355: 4330: 4310: 4297: 4292: 2502: 1439: 1349: 694: 671: 659: 614: 571: 534: 527: 449: 365: 359: 282: 207: 201: 196: 65: 4411: 1846:
of the center of mass is constant, from which follows that the total momentum
761: 4483: 4088: 3593:{\displaystyle E={\frac {1}{2}}\mu {\dot {\mathbf {r} }}^{2}+U(\mathbf {r} )} 3211: 899:{\displaystyle {\boldsymbol {r}}={\boldsymbol {x}}_{1}-{\boldsymbol {x}}_{2}} 603: 454: 287: 244: 733:
to the section by replacing the section with a link and a summary or by
4474: 4287: 4272: 2876: 2289: 172: 162: 157: 69: 721:
Classical central-force problem#Relation to the classical two-body problem
4248:{\displaystyle \mu {\ddot {\mathbf {r} }}={F}(r){\hat {\mathbf {r} }}\ ,} 4181: 336: 78: 4402: 3170:
Introducing the assumption (true of most physical forces, as they obey
1443: 1353: 667: 663: 416: 372: 331: 109: 61: 755: 538: 81:(in which the barycenter is external to both bodies), as well as the 4146:{\displaystyle \mathbf {F} (\mathbf {r} )=F(r){\hat {\mathbf {r} }}} 2792:
of the system, with respect to the center of mass, by the equations
1892: 1446:) of the system. Addition of the force equations (1) and (2) yields 560: 3721:{\displaystyle \mathbf {x} _{2}=-{\frac {\mu }{m_{2}}}\mathbf {r} } 655: 643: 3665:{\displaystyle \mathbf {x} _{1}={\frac {\mu }{m_{1}}}\mathbf {r} } 682: 599: 2530:
have been determined, the original trajectories may be obtained
1324:
is the force on mass 1 due to its interactions with mass 2, and
589: 89:
system (in which the barycenter is internal to the larger body).
2914: 1411: 542: 546: 137: 82: 23:. For the career management problem of working couples, see 991:
be their masses. The goal is to determine the trajectories
86: 57: 3750:
that separately contain the kinetic energy of each body:
44: 35: 609:
For the derivation of the solutions to the problem, see
595:
influences will be small enough to be ignored safely).
2751:
as may be verified by substituting the definitions of
4190: 4097: 3756: 3677: 3624: 3532: 3267: 3077: 2927: 2798: 2646: 2536: 2470: 2437: 2298: 2273: 2172: 1903: 1807: 1770: 1635: 1452: 1422: 1211: 1097: 912: 860: 774: 658:
in an atom are sometimes described as "orbiting" its
4401: 4410: 4371: 4263:) is negative in the case of an attractive force. 4247: 4145: 4055: 3720: 3664: 3592: 3512: 3138: 3031: 2861: 2759:into the right-hand sides of these two equations. 2743: 2633: 2489: 2456: 2410: 2279: 2259: 2098: 1838: 1793: 1754: 1602: 1430: 1293: 1179: 947: 898: 846: 1893:Displacement vector motion (2nd one-body problem) 4481: 4331:"The Sturm-Liouville problem of two-body system" 3223: 3198:(conserved). Therefore, the displacement vector 644:Inapplicability to atoms and subatomic particles 977:be the vector positions of the two bodies, and 683:Reduction to two independent, one-body problems 4369: 584: 2907:) the rate of change of the angular momentum 1839:{\displaystyle \mathbf {v} ={\frac {dR}{dt}}} 768:for two-body problem; Jacobi coordinates are 633:are isolated enough from their surroundings. 590:Gravitation and other inverse-square examples 499: 2762: 1412:Center of mass motion (1st one-body problem) 4435: 3526:is the lowest and the total energy becomes 2490:{\displaystyle \mathbf {F} (\mathbf {r} )} 2457:{\displaystyle \mathbf {F} (\mathbf {r} )} 506: 492: 4354: 2135:from mass 2 to mass 1, as defined above. 1794:{\displaystyle {\ddot {\mathbf {R} }}=0} 1348:) results in an equation describing the 760: 4363: 886: 871: 862: 834: 802: 776: 4482: 4076:For many physical problems, the force 561:reduced to a pair of one-body problems 21:Two-body problem in general relativity 4378:. Springer. p. 58; Figure 2.15. 16:Motion problem in classical mechanics 2144:and not of their absolute positions 1202: 1088: 698: 4328: 3172:Newton's strong third law of motion 13: 14: 4506: 4475:Eric Weisstein's World of Physics 4464: 4335:Journal of Physics Communications 4065: 670:(this is the source of the term " 552:A simpler "one body" model, the " 278:Kepler's laws of planetary motion 4229: 4198: 4133: 4107: 4099: 3998: 3950: 3874: 3826: 3728:and in a similar way the energy 3714: 3680: 3658: 3627: 3583: 3557: 3522:In the center of mass frame the 3503: 3477: 3440: 3386: 3355: 3306: 3126: 3118: 3099: 3079: 3069:pointing in the same direction, 3013: 2999: 2985: 2965: 2943: 2929: 2841: 2824: 2816: 2808: 2800: 2728: 2672: 2649: 2618: 2562: 2539: 2480: 2472: 2447: 2439: 2250: 2242: 2225: 2210: 2195: 2180: 2162:; otherwise, there would not be 2086: 2007: 1978: 1950: 1926: 1908: 1809: 1775: 1705: 1671: 1640: 1584: 1569: 1554: 1502: 1468: 1424: 1275: 1244: 1229: 1214: 1161: 1130: 1115: 1100: 1082:When applied to the two masses, 703: 108: 43: 34: 4395: 4072:Classical central-force problem 948:{\displaystyle M=m_{1}+m_{2}\ } 611:Classical central-force problem 4322: 4233: 4222: 4216: 4137: 4126: 4120: 4111: 4103: 4002: 3994: 3878: 3870: 3587: 3579: 3507: 3499: 3432: 3406: 3390: 3382: 3039:and using the property of the 2738: 2732: 2682: 2676: 2665: 2659: 2628: 2622: 2572: 2566: 2555: 2549: 2484: 2476: 2451: 2443: 2254: 2246: 2235: 2205: 1547: 1521: 1254: 1224: 1140: 1110: 1023:, given the initial positions 64:external to both bodies, with 1: 4316: 3224:Energy of the two-body system 1431:{\displaystyle \mathbf {R} } 7: 4445:(2nd. ed.). New York: 4417:(3rd. ed.). New York: 4329:Luo, Siwei (22 June 2020). 4266: 3732:is related to the energies 1344: 1307: 1193: 1051:and the initial velocities 717:the scope of other articles 585:Results for prominent cases 432:Tsiolkovsky rocket equation 68:. This model is typical of 10: 4511: 4283:Euler's three-body problem 4091:, i.e., it is of the form 4069: 692: 686: 570:(and, more generally, the 401:Engineering and efficiency 220:Bi-elliptic transfer orbit 18: 2885:is the relative position 2763:Two-body motion is planar 2420:Solving the equation for 2106:where we have again used 25:Two-body problem (career) 4356:10.1088/2399-6528/ab9c30 3210:are always in the plane 3190:angular momentum vector 1876:conservation of momentum 1801:shows that the velocity 1764:The resulting equation: 638:Sturm-Liouville equation 630:electrostatic attraction 427:Propellant mass fraction 326:Gravitational influences 4370:David Betounes (2001). 3214:to the constant vector 1878:). Hence, the position 1438:be the position of the 1356:) motion. By contrast, 298:Specific orbital energy 4374:Differential Equations 4278:Equation of the center 4249: 4147: 4057: 3722: 3666: 3594: 3514: 3243:then the system has a 3140: 3033: 2863: 2745: 2635: 2491: 2458: 2412: 2281: 2261: 2164:translational symmetry 2100: 1840: 1795: 1756: 1604: 1432: 1295: 1181: 956: 949: 900: 848: 215:Hohmann transfer orbit 56:Two bodies of similar 4250: 4180:is the corresponding 4148: 4058: 3723: 3667: 3595: 3515: 3141: 3034: 2864: 2746: 2636: 2492: 2464:. For the case where 2459: 2413: 2282: 2262: 2101: 1841: 1796: 1757: 1605: 1433: 1296: 1182: 950: 901: 849: 764: 735:splitting the content 729:and help introduce a 554:central-force problem 411:Preflight engineering 143:Argument of periapsis 4188: 4095: 3754: 3675: 3622: 3618:can be expressed as 3530: 3265: 3075: 3041:vector cross product 2925: 2796: 2774:Proof: Defining the 2769:center of mass frame 2644: 2534: 2468: 2435: 2296: 2280:{\displaystyle \mu } 2271: 2170: 1901: 1805: 1768: 1633: 1450: 1420: 1209: 1095: 910: 858: 772: 467:Propulsive maneuvers 4442:Classical Mechanics 4347:2020JPhCo...4f1001L 3970: 3846: 3375: 3326: 2133:displacement vector 1610:where we have used 1342:equations (1) and ( 1084:Newton's second law 737:into a new article. 598:Under the force of 520:classical mechanics 444:Efficiency measures 347:Sphere of influence 316:Celestial mechanics 98:Part of a series on 79:Pluto–Charon system 4306:Three-body problem 4245: 4143: 4053: 4051: 3945: 3821: 3718: 3662: 3590: 3510: 3350: 3301: 3261:can be written as 3136: 3029: 2859: 2741: 2631: 2499:inverse-square law 2487: 2454: 2408: 2277: 2257: 2108:Newton's third law 2096: 1874:is also constant ( 1836: 1791: 1752: 1612:Newton's third law 1600: 1428: 1291: 1177: 957: 945: 896: 844: 766:Jacobi coordinates 727:discuss this issue 626:inverse-square law 622:scalar force field 568:three-body problem 263:Dynamical friction 60:orbiting a common 4495:Dynamical systems 4241: 4236: 4205: 4140: 4016: 3989: 3957: 3933: 3917: 3865: 3833: 3809: 3793: 3711: 3655: 3564: 3547: 3484: 3467: 3447: 3404: 3362: 3338: 3313: 3289: 3275: 3204:and its velocity 3132: 3112: 3091: 3085: 3025: 3020: 2992: 2972: 2956: 2854: 2725: 2615: 2403: 2349: 2346: 2326: 2187: 2077: 2057: 2027: 1998: 1957: 1933: 1915: 1834: 1782: 1747: 1712: 1678: 1647: 1561: 1509: 1475: 1315: 1314: 1282: 1201: 1200: 1168: 944: 830: 798: 752: 751: 676:quantum mechanics 566:By contrast, the 516: 515: 366:Lagrangian points 303:Vis-viva equation 273:Kepler's equation 120:Orbital mechanics 4502: 4471:Two-body problem 4460: 4432: 4416: 4390: 4389: 4377: 4367: 4361: 4360: 4358: 4326: 4254: 4252: 4251: 4246: 4239: 4238: 4237: 4232: 4227: 4215: 4207: 4206: 4201: 4196: 4179: 4165: 4163: 4152: 4150: 4149: 4144: 4142: 4141: 4136: 4131: 4110: 4102: 4086: 4062: 4060: 4059: 4054: 4052: 4048: 4047: 4035: 4034: 4018: 4017: 4014: 4001: 3990: 3988: 3987: 3975: 3969: 3964: 3959: 3958: 3953: 3948: 3944: 3943: 3934: 3926: 3918: 3916: 3915: 3903: 3894: 3893: 3877: 3866: 3864: 3863: 3851: 3845: 3840: 3835: 3834: 3829: 3824: 3820: 3819: 3810: 3802: 3794: 3792: 3791: 3779: 3770: 3769: 3749: 3740: 3727: 3725: 3724: 3719: 3717: 3712: 3710: 3709: 3697: 3689: 3688: 3683: 3671: 3669: 3668: 3663: 3661: 3656: 3654: 3653: 3641: 3636: 3635: 3630: 3617: 3608: 3600:The coordinates 3599: 3597: 3596: 3591: 3586: 3572: 3571: 3566: 3565: 3560: 3555: 3548: 3540: 3519: 3517: 3516: 3511: 3506: 3492: 3491: 3486: 3485: 3480: 3475: 3468: 3460: 3455: 3454: 3449: 3448: 3443: 3438: 3431: 3430: 3418: 3417: 3405: 3397: 3389: 3374: 3369: 3364: 3363: 3358: 3353: 3349: 3348: 3339: 3331: 3325: 3320: 3315: 3314: 3309: 3304: 3300: 3299: 3290: 3282: 3277: 3276: 3273: 3256: 3245:potential energy 3238: 3219: 3209: 3203: 3195: 3187: 3166: 3145: 3143: 3142: 3137: 3130: 3129: 3121: 3113: 3111: 3103: 3102: 3093: 3089: 3083: 3082: 3068: 3062: 3057:for any vectors 3056: 3038: 3036: 3035: 3030: 3023: 3022: 3021: 3016: 3011: 3002: 2994: 2993: 2988: 2983: 2974: 2973: 2968: 2963: 2957: 2955: 2947: 2946: 2937: 2932: 2921: 2912: 2906: 2900: 2884: 2874: 2868: 2866: 2865: 2860: 2855: 2853: 2845: 2844: 2835: 2827: 2819: 2811: 2803: 2791: 2785:angular momentum 2782: 2750: 2748: 2747: 2742: 2731: 2726: 2724: 2723: 2722: 2710: 2709: 2699: 2698: 2689: 2675: 2658: 2657: 2652: 2640: 2638: 2637: 2632: 2621: 2616: 2614: 2613: 2612: 2600: 2599: 2589: 2588: 2579: 2565: 2548: 2547: 2542: 2529: 2518: 2496: 2494: 2493: 2488: 2483: 2475: 2463: 2461: 2460: 2455: 2450: 2442: 2430: 2417: 2415: 2414: 2409: 2404: 2402: 2401: 2400: 2388: 2387: 2377: 2376: 2375: 2366: 2365: 2355: 2350: 2348: 2347: 2345: 2344: 2332: 2327: 2325: 2324: 2312: 2306: 2286: 2284: 2283: 2278: 2266: 2264: 2263: 2258: 2253: 2245: 2234: 2233: 2228: 2219: 2218: 2213: 2204: 2203: 2198: 2189: 2188: 2183: 2178: 2161: 2152: 2143: 2130: 2124: 2105: 2103: 2102: 2097: 2095: 2094: 2089: 2083: 2079: 2078: 2076: 2075: 2063: 2058: 2056: 2055: 2043: 2033: 2029: 2028: 2026: 2025: 2016: 2015: 2010: 2004: 1999: 1997: 1996: 1987: 1986: 1981: 1975: 1965: 1964: 1959: 1958: 1953: 1948: 1941: 1940: 1935: 1934: 1929: 1924: 1917: 1916: 1911: 1906: 1888: 1873: 1845: 1843: 1842: 1837: 1835: 1833: 1825: 1817: 1812: 1800: 1798: 1797: 1792: 1784: 1783: 1778: 1773: 1761: 1759: 1758: 1753: 1748: 1746: 1745: 1744: 1732: 1731: 1721: 1720: 1719: 1714: 1713: 1708: 1703: 1699: 1698: 1686: 1685: 1680: 1679: 1674: 1669: 1665: 1664: 1654: 1649: 1648: 1643: 1638: 1628: 1609: 1607: 1606: 1601: 1593: 1592: 1587: 1578: 1577: 1572: 1563: 1562: 1557: 1552: 1546: 1545: 1533: 1532: 1517: 1516: 1511: 1510: 1505: 1500: 1496: 1495: 1483: 1482: 1477: 1476: 1471: 1466: 1462: 1461: 1437: 1435: 1434: 1429: 1427: 1407: 1393: 1379: 1309: 1300: 1298: 1297: 1292: 1290: 1289: 1284: 1283: 1278: 1273: 1269: 1268: 1253: 1252: 1247: 1238: 1237: 1232: 1223: 1222: 1217: 1203: 1195: 1186: 1184: 1183: 1178: 1176: 1175: 1170: 1169: 1164: 1159: 1155: 1154: 1139: 1138: 1133: 1124: 1123: 1118: 1109: 1108: 1103: 1089: 1078: 1064: 1050: 1036: 1018: 1004: 976: 967: 954: 952: 951: 946: 942: 941: 940: 928: 927: 905: 903: 902: 897: 895: 894: 889: 880: 879: 874: 865: 853: 851: 850: 845: 843: 842: 837: 831: 826: 825: 816: 811: 810: 805: 799: 794: 793: 784: 779: 747: 744: 738: 707: 706: 699: 664:early conjecture 524:two-body problem 508: 501: 494: 473:Orbital maneuver 422:Payload fraction 402: 383:Lissajous orbits 317: 288:Orbital velocity 235:Hyperbolic orbit 131:Orbital elements 121: 112: 95: 94: 47: 38: 4510: 4509: 4505: 4504: 4503: 4501: 4500: 4499: 4480: 4479: 4467: 4457: 4429: 4398: 4393: 4386: 4368: 4364: 4327: 4323: 4319: 4269: 4228: 4226: 4225: 4211: 4197: 4195: 4194: 4189: 4186: 4185: 4184:. We now have: 4167: 4159: 4154: 4132: 4130: 4129: 4106: 4098: 4096: 4093: 4092: 4077: 4074: 4068: 4050: 4049: 4043: 4039: 4030: 4026: 4019: 4013: 4009: 4006: 4005: 3997: 3983: 3979: 3974: 3965: 3960: 3949: 3947: 3946: 3939: 3935: 3925: 3911: 3907: 3902: 3895: 3889: 3885: 3882: 3881: 3873: 3859: 3855: 3850: 3841: 3836: 3825: 3823: 3822: 3815: 3811: 3801: 3787: 3783: 3778: 3771: 3765: 3761: 3757: 3755: 3752: 3751: 3748: 3742: 3739: 3733: 3713: 3705: 3701: 3696: 3684: 3679: 3678: 3676: 3673: 3672: 3657: 3649: 3645: 3640: 3631: 3626: 3625: 3623: 3620: 3619: 3616: 3610: 3607: 3601: 3582: 3567: 3556: 3554: 3553: 3552: 3539: 3531: 3528: 3527: 3502: 3487: 3476: 3474: 3473: 3472: 3459: 3450: 3439: 3437: 3436: 3435: 3426: 3422: 3413: 3409: 3396: 3385: 3370: 3365: 3354: 3352: 3351: 3344: 3340: 3330: 3321: 3316: 3305: 3303: 3302: 3295: 3291: 3281: 3272: 3268: 3266: 3263: 3262: 3257:, so the total 3247: 3229: 3226: 3215: 3205: 3199: 3191: 3175: 3147: 3125: 3117: 3104: 3098: 3094: 3092: 3078: 3076: 3073: 3072: 3064: 3058: 3044: 3012: 3010: 3009: 2998: 2984: 2982: 2981: 2964: 2962: 2961: 2948: 2942: 2938: 2936: 2928: 2926: 2923: 2922: 2917: 2913:equals the net 2908: 2902: 2899: 2892: 2886: 2880: 2872: 2846: 2840: 2836: 2834: 2823: 2815: 2807: 2799: 2797: 2794: 2793: 2787: 2778: 2776:linear momentum 2765: 2727: 2718: 2714: 2705: 2701: 2700: 2694: 2690: 2688: 2671: 2653: 2648: 2647: 2645: 2642: 2641: 2617: 2608: 2604: 2595: 2591: 2590: 2584: 2580: 2578: 2561: 2543: 2538: 2537: 2535: 2532: 2531: 2520: 2509: 2479: 2471: 2469: 2466: 2465: 2446: 2438: 2436: 2433: 2432: 2421: 2396: 2392: 2383: 2379: 2378: 2371: 2367: 2361: 2357: 2356: 2354: 2340: 2336: 2331: 2320: 2316: 2311: 2310: 2305: 2297: 2294: 2293: 2272: 2269: 2268: 2249: 2241: 2229: 2224: 2223: 2214: 2209: 2208: 2199: 2194: 2193: 2179: 2177: 2176: 2171: 2168: 2167: 2160: 2154: 2151: 2145: 2139: 2126: 2123: 2116: 2110: 2090: 2085: 2084: 2071: 2067: 2062: 2051: 2047: 2042: 2041: 2037: 2021: 2017: 2011: 2006: 2005: 2003: 1992: 1988: 1982: 1977: 1976: 1974: 1973: 1969: 1960: 1949: 1947: 1946: 1945: 1936: 1925: 1923: 1922: 1921: 1907: 1905: 1904: 1902: 1899: 1898: 1895: 1879: 1872: 1866: 1859: 1853: 1847: 1826: 1818: 1816: 1808: 1806: 1803: 1802: 1774: 1772: 1771: 1769: 1766: 1765: 1740: 1736: 1727: 1723: 1722: 1715: 1704: 1702: 1701: 1700: 1694: 1690: 1681: 1670: 1668: 1667: 1666: 1660: 1656: 1655: 1653: 1639: 1637: 1636: 1634: 1631: 1630: 1627: 1620: 1614: 1588: 1583: 1582: 1573: 1568: 1567: 1553: 1551: 1550: 1541: 1537: 1528: 1524: 1512: 1501: 1499: 1498: 1497: 1491: 1487: 1478: 1467: 1465: 1464: 1463: 1457: 1453: 1451: 1448: 1447: 1423: 1421: 1418: 1417: 1414: 1401: 1395: 1387: 1381: 1378: 1371: 1361: 1330: 1323: 1285: 1274: 1272: 1271: 1270: 1264: 1260: 1248: 1243: 1242: 1233: 1228: 1227: 1218: 1213: 1212: 1210: 1207: 1206: 1171: 1160: 1158: 1157: 1156: 1150: 1146: 1134: 1129: 1128: 1119: 1114: 1113: 1104: 1099: 1098: 1096: 1093: 1092: 1072: 1066: 1058: 1052: 1044: 1038: 1030: 1024: 1012: 1006: 998: 992: 990: 983: 975: 969: 966: 960: 936: 932: 923: 919: 911: 908: 907: 890: 885: 884: 875: 870: 869: 861: 859: 856: 855: 838: 833: 832: 821: 817: 815: 806: 801: 800: 789: 785: 783: 775: 773: 770: 769: 748: 742: 739: 724: 719:, specifically 708: 704: 697: 691: 685: 662:, following an 646: 592: 587: 528:point particles 512: 483: 482: 478:Orbit insertion 468: 460: 459: 445: 437: 436: 412: 404: 400: 393: 392: 388:Lyapunov orbits 379: 378: 362: 352: 351: 327: 319: 315: 308: 307: 293:Surface gravity 268:Escape velocity 258: 250: 249: 230:Parabolic orbit 226: 225: 192: 190: 187:two-body orbits 178: 177: 168:Semi-major axis 133: 123: 119: 93: 92: 91: 90: 73: 66:elliptic orbits 50: 49: 48: 40: 39: 28: 17: 12: 11: 5: 4508: 4498: 4497: 4492: 4478: 4477: 4466: 4465:External links 4463: 4462: 4461: 4455: 4447:Addison-Wesley 4433: 4427: 4419:Pergamon Press 4397: 4394: 4392: 4391: 4384: 4362: 4320: 4318: 4315: 4314: 4313: 4311:Virial theorem 4308: 4303: 4295: 4293:Kepler problem 4290: 4285: 4280: 4275: 4268: 4265: 4244: 4235: 4231: 4224: 4221: 4218: 4214: 4210: 4204: 4200: 4193: 4139: 4135: 4128: 4125: 4122: 4119: 4116: 4113: 4109: 4105: 4101: 4070:Main article: 4067: 4066:Central forces 4064: 4046: 4042: 4038: 4033: 4029: 4025: 4022: 4020: 4012: 4008: 4007: 4004: 4000: 3996: 3993: 3986: 3982: 3978: 3973: 3968: 3963: 3956: 3952: 3942: 3938: 3932: 3929: 3924: 3921: 3914: 3910: 3906: 3901: 3898: 3896: 3892: 3888: 3884: 3883: 3880: 3876: 3872: 3869: 3862: 3858: 3854: 3849: 3844: 3839: 3832: 3828: 3818: 3814: 3808: 3805: 3800: 3797: 3790: 3786: 3782: 3777: 3774: 3772: 3768: 3764: 3760: 3759: 3746: 3737: 3716: 3708: 3704: 3700: 3695: 3692: 3687: 3682: 3660: 3652: 3648: 3644: 3639: 3634: 3629: 3614: 3605: 3589: 3585: 3581: 3578: 3575: 3570: 3563: 3559: 3551: 3546: 3543: 3538: 3535: 3524:kinetic energy 3509: 3505: 3501: 3498: 3495: 3490: 3483: 3479: 3471: 3466: 3463: 3458: 3453: 3446: 3442: 3434: 3429: 3425: 3421: 3416: 3412: 3408: 3403: 3400: 3395: 3392: 3388: 3384: 3381: 3378: 3373: 3368: 3361: 3357: 3347: 3343: 3337: 3334: 3329: 3324: 3319: 3312: 3308: 3298: 3294: 3288: 3285: 3280: 3271: 3225: 3222: 3135: 3128: 3124: 3120: 3116: 3110: 3107: 3101: 3097: 3088: 3081: 3028: 3019: 3015: 3008: 3005: 3001: 2997: 2991: 2987: 2980: 2977: 2971: 2967: 2960: 2954: 2951: 2945: 2941: 2935: 2931: 2897: 2890: 2858: 2852: 2849: 2843: 2839: 2833: 2830: 2826: 2822: 2818: 2814: 2810: 2806: 2802: 2764: 2761: 2740: 2737: 2734: 2730: 2721: 2717: 2713: 2708: 2704: 2697: 2693: 2687: 2684: 2681: 2678: 2674: 2670: 2667: 2664: 2661: 2656: 2651: 2630: 2627: 2624: 2620: 2611: 2607: 2603: 2598: 2594: 2587: 2583: 2577: 2574: 2571: 2568: 2564: 2560: 2557: 2554: 2551: 2546: 2541: 2503:Kepler problem 2486: 2482: 2478: 2474: 2453: 2449: 2445: 2441: 2407: 2399: 2395: 2391: 2386: 2382: 2374: 2370: 2364: 2360: 2353: 2343: 2339: 2335: 2330: 2323: 2319: 2315: 2309: 2304: 2301: 2276: 2256: 2252: 2248: 2244: 2240: 2237: 2232: 2227: 2222: 2217: 2212: 2207: 2202: 2197: 2192: 2186: 2182: 2175: 2158: 2149: 2121: 2114: 2093: 2088: 2082: 2074: 2070: 2066: 2061: 2054: 2050: 2046: 2040: 2036: 2032: 2024: 2020: 2014: 2009: 2002: 1995: 1991: 1985: 1980: 1972: 1968: 1963: 1956: 1952: 1944: 1939: 1932: 1928: 1920: 1914: 1910: 1894: 1891: 1870: 1864: 1857: 1851: 1832: 1829: 1824: 1821: 1815: 1811: 1790: 1787: 1781: 1777: 1751: 1743: 1739: 1735: 1730: 1726: 1718: 1711: 1707: 1697: 1693: 1689: 1684: 1677: 1673: 1663: 1659: 1652: 1646: 1642: 1625: 1618: 1599: 1596: 1591: 1586: 1581: 1576: 1571: 1566: 1560: 1556: 1549: 1544: 1540: 1536: 1531: 1527: 1523: 1520: 1515: 1508: 1504: 1494: 1490: 1486: 1481: 1474: 1470: 1460: 1456: 1440:center of mass 1426: 1413: 1410: 1399: 1385: 1376: 1369: 1350:center of mass 1328: 1321: 1313: 1312: 1303: 1301: 1288: 1281: 1277: 1267: 1263: 1259: 1256: 1251: 1246: 1241: 1236: 1231: 1226: 1221: 1216: 1199: 1198: 1189: 1187: 1174: 1167: 1163: 1153: 1149: 1145: 1142: 1137: 1132: 1127: 1122: 1117: 1112: 1107: 1102: 1070: 1056: 1042: 1028: 1019:for all times 1010: 996: 988: 981: 973: 964: 939: 935: 931: 926: 922: 918: 915: 893: 888: 883: 878: 873: 868: 864: 841: 836: 829: 824: 820: 814: 809: 804: 797: 792: 788: 782: 778: 750: 749: 711: 709: 702: 695:Kepler problem 684: 681: 645: 642: 615:Kepler problem 604:conic sections 591: 588: 586: 583: 535:Kepler problem 514: 513: 511: 510: 503: 496: 488: 485: 484: 481: 480: 475: 469: 466: 465: 462: 461: 458: 457: 452: 450:Gravity assist 446: 443: 442: 439: 438: 435: 434: 429: 424: 419: 413: 410: 409: 406: 405: 398: 395: 394: 391: 390: 385: 377: 376: 368: 364: 363: 358: 357: 354: 353: 350: 349: 344: 339: 334: 328: 325: 324: 321: 320: 313: 310: 309: 306: 305: 300: 295: 290: 285: 283:Orbital period 280: 275: 270: 265: 259: 256: 255: 252: 251: 248: 247: 245:Decaying orbit 242: 237: 232: 224: 223: 217: 210: 208:Transfer orbit 206: 205: 204: 202:Elliptic orbit 199: 197:Circular orbit 193: 184: 183: 180: 179: 176: 175: 170: 165: 160: 155: 150: 145: 140: 134: 129: 128: 125: 124: 117: 114: 113: 105: 104: 100: 99: 52: 51: 42: 41: 33: 32: 31: 30: 29: 15: 9: 6: 4: 3: 2: 4507: 4496: 4493: 4491: 4488: 4487: 4485: 4476: 4472: 4469: 4468: 4458: 4456:0-201-02918-9 4452: 4448: 4444: 4443: 4438: 4434: 4430: 4428:0-08-029141-4 4424: 4420: 4415: 4414: 4408: 4404: 4400: 4399: 4387: 4385:0-387-95140-7 4381: 4376: 4375: 4366: 4357: 4352: 4348: 4344: 4341:(6): 061001. 4340: 4336: 4332: 4325: 4321: 4312: 4309: 4307: 4304: 4302: 4301:-body problem 4300: 4296: 4294: 4291: 4289: 4286: 4284: 4281: 4279: 4276: 4274: 4271: 4270: 4264: 4262: 4258: 4242: 4219: 4212: 4208: 4202: 4191: 4183: 4178: 4174: 4170: 4162: 4157: 4123: 4117: 4114: 4090: 4089:central force 4084: 4080: 4073: 4063: 4044: 4040: 4036: 4031: 4027: 4023: 4021: 4010: 3991: 3984: 3980: 3976: 3971: 3966: 3961: 3954: 3940: 3936: 3930: 3927: 3922: 3919: 3912: 3908: 3904: 3899: 3897: 3890: 3886: 3867: 3860: 3856: 3852: 3847: 3842: 3837: 3830: 3816: 3812: 3806: 3803: 3798: 3795: 3788: 3784: 3780: 3775: 3773: 3766: 3762: 3745: 3736: 3731: 3706: 3702: 3698: 3693: 3690: 3685: 3650: 3646: 3642: 3637: 3632: 3613: 3604: 3576: 3573: 3568: 3561: 3549: 3544: 3541: 3536: 3533: 3525: 3520: 3496: 3493: 3488: 3481: 3469: 3464: 3461: 3456: 3451: 3444: 3427: 3423: 3419: 3414: 3410: 3401: 3398: 3393: 3379: 3376: 3371: 3366: 3359: 3345: 3341: 3335: 3332: 3327: 3322: 3317: 3310: 3296: 3292: 3286: 3283: 3278: 3269: 3260: 3254: 3250: 3246: 3242: 3236: 3232: 3228:If the force 3221: 3218: 3213: 3212:perpendicular 3208: 3202: 3197: 3194: 3186: 3182: 3178: 3173: 3168: 3165: 3161: 3158: 3154: 3150: 3133: 3122: 3114: 3108: 3105: 3095: 3086: 3070: 3067: 3061: 3055: 3051: 3047: 3042: 3026: 3017: 3006: 3003: 2995: 2989: 2978: 2975: 2969: 2958: 2952: 2949: 2939: 2933: 2920: 2916: 2911: 2905: 2896: 2889: 2883: 2878: 2869: 2856: 2850: 2847: 2837: 2831: 2828: 2820: 2812: 2804: 2790: 2786: 2781: 2777: 2772: 2770: 2760: 2758: 2754: 2735: 2719: 2715: 2711: 2706: 2702: 2695: 2691: 2685: 2679: 2668: 2662: 2654: 2625: 2609: 2605: 2601: 2596: 2592: 2585: 2581: 2575: 2569: 2558: 2552: 2544: 2527: 2523: 2516: 2512: 2506: 2504: 2500: 2428: 2424: 2418: 2405: 2397: 2393: 2389: 2384: 2380: 2372: 2368: 2362: 2358: 2351: 2341: 2337: 2333: 2328: 2321: 2317: 2313: 2307: 2302: 2299: 2292: 2291: 2274: 2238: 2230: 2220: 2215: 2200: 2190: 2184: 2173: 2165: 2157: 2148: 2142: 2136: 2134: 2129: 2120: 2113: 2109: 2091: 2080: 2072: 2068: 2064: 2059: 2052: 2048: 2044: 2038: 2034: 2030: 2022: 2018: 2012: 2000: 1993: 1989: 1983: 1970: 1966: 1961: 1954: 1942: 1937: 1930: 1918: 1912: 1890: 1886: 1882: 1877: 1869: 1863: 1856: 1850: 1830: 1827: 1822: 1819: 1813: 1788: 1785: 1779: 1762: 1749: 1741: 1737: 1733: 1728: 1724: 1716: 1709: 1695: 1691: 1687: 1682: 1675: 1661: 1657: 1650: 1644: 1624: 1617: 1613: 1597: 1594: 1589: 1579: 1574: 1564: 1558: 1542: 1538: 1534: 1529: 1525: 1518: 1513: 1506: 1492: 1488: 1484: 1479: 1472: 1458: 1454: 1445: 1441: 1409: 1405: 1398: 1391: 1384: 1375: 1368: 1364: 1359: 1355: 1351: 1347: 1346: 1341: 1336: 1334: 1327: 1320: 1311: 1304: 1302: 1286: 1279: 1265: 1261: 1257: 1249: 1239: 1234: 1219: 1205: 1204: 1197: 1190: 1188: 1172: 1165: 1151: 1147: 1143: 1135: 1125: 1120: 1105: 1091: 1090: 1087: 1085: 1080: 1076: 1069: 1062: 1055: 1048: 1041: 1034: 1027: 1022: 1016: 1009: 1002: 995: 987: 980: 972: 963: 937: 933: 929: 924: 920: 916: 913: 891: 881: 876: 866: 839: 827: 822: 818: 812: 807: 795: 790: 786: 780: 767: 763: 759: 757: 746: 736: 732: 731:summary style 728: 722: 718: 716: 712:This section 710: 701: 700: 696: 690: 680: 677: 673: 669: 665: 661: 657: 653: 651: 641: 639: 634: 631: 627: 623: 618: 616: 612: 607: 605: 601: 596: 582: 580: 576: 575:-body problem 574: 569: 564: 562: 557: 555: 550: 548: 544: 540: 536: 531: 529: 525: 521: 509: 504: 502: 497: 495: 490: 489: 487: 486: 479: 476: 474: 471: 470: 464: 463: 456: 455:Oberth effect 453: 451: 448: 447: 441: 440: 433: 430: 428: 425: 423: 420: 418: 415: 414: 408: 407: 403: 397: 396: 389: 386: 384: 381: 380: 374: 370: 369: 367: 361: 360:N-body orbits 356: 355: 348: 345: 343: 342:Perturbations 340: 338: 335: 333: 330: 329: 323: 322: 318: 312: 311: 304: 301: 299: 296: 294: 291: 289: 286: 284: 281: 279: 276: 274: 271: 269: 266: 264: 261: 260: 254: 253: 246: 243: 241: 238: 236: 233: 231: 228: 227: 221: 218: 216: 212: 211: 209: 203: 200: 198: 195: 194: 188: 182: 181: 174: 171: 169: 166: 164: 163:Orbital nodes 161: 159: 156: 154: 151: 149: 146: 144: 141: 139: 136: 135: 132: 127: 126: 122: 116: 115: 111: 107: 106: 103:Astrodynamics 102: 101: 97: 96: 88: 84: 80: 76: 71: 67: 63: 59: 55: 46: 37: 26: 22: 4440: 4412: 4396:Bibliography 4373: 4365: 4338: 4334: 4324: 4298: 4288:Kepler orbit 4273:Energy drift 4260: 4256: 4176: 4172: 4168: 4160: 4155: 4082: 4078: 4075: 3743: 3734: 3729: 3611: 3602: 3521: 3252: 3248: 3241:conservative 3234: 3230: 3227: 3216: 3206: 3200: 3192: 3184: 3180: 3176: 3169: 3163: 3159: 3156: 3152: 3148: 3071: 3065: 3059: 3053: 3049: 3045: 2918: 2909: 2903: 2894: 2887: 2881: 2877:reduced mass 2870: 2788: 2779: 2773: 2766: 2756: 2752: 2525: 2521: 2514: 2510: 2507: 2426: 2422: 2419: 2290:reduced mass 2288: 2155: 2146: 2140: 2137: 2127: 2118: 2111: 1896: 1884: 1880: 1867: 1861: 1854: 1848: 1763: 1622: 1615: 1415: 1403: 1396: 1389: 1382: 1373: 1366: 1362: 1357: 1343: 1339: 1337: 1332: 1325: 1318: 1316: 1305: 1191: 1086:states that 1081: 1074: 1067: 1060: 1053: 1046: 1039: 1032: 1025: 1020: 1014: 1007: 1000: 993: 985: 978: 970: 961: 958: 753: 740: 713: 654: 649: 647: 635: 619: 608: 597: 593: 578: 572: 565: 558: 551: 532: 523: 517: 240:Radial orbit 191:eccentricity 186: 173:True anomaly 158:Mean anomaly 148:Eccentricity 74: 70:binary stars 53: 4437:Goldstein H 4407:Lifshitz EM 4182:unit vector 3196:is constant 2497:follows an 1358:subtracting 624:obeying an 373:Halo orbits 337:Hill sphere 153:Inclination 4484:Categories 4317:References 2501:, see the 2125:and where 1629:and where 1444:barycenter 1354:barycenter 1306:(Equation 1192:(Equation 715:duplicates 693:See also: 687:See also: 668:Niels Bohr 539:satellites 417:Mass ratio 332:Barycenter 62:barycenter 4413:Mechanics 4403:Landau LD 4234:^ 4203:¨ 4192:μ 4138:^ 3977:μ 3955:˙ 3905:μ 3853:μ 3831:˙ 3781:μ 3699:μ 3694:− 3643:μ 3562:˙ 3550:μ 3482:˙ 3470:μ 3445:˙ 3360:˙ 3311:˙ 3123:× 3018:¨ 3007:μ 3004:× 2990:˙ 2979:μ 2976:× 2970:˙ 2832:μ 2829:× 2813:× 2686:− 2300:μ 2275:μ 2185:¨ 2174:μ 2001:− 1955:¨ 1943:− 1931:¨ 1913:¨ 1780:¨ 1710:¨ 1676:¨ 1651:≡ 1645:¨ 1559:¨ 1507:¨ 1473:¨ 1280:¨ 1166:¨ 882:− 756:potential 743:June 2019 656:Electrons 257:Equations 185:Types of 4439:(1980). 4409:(1976). 4267:See also 4158:= | 3188:and the 2783:and the 4343:Bibcode 3155:  2875:is the 2287:is the 2131:is the 725:Please 672:orbital 660:nucleus 628:, with 600:gravity 543:planets 4490:Orbits 4453:  4425:  4382:  4255:where 4240:  4164:| 4153:where 3259:energy 3131:  3090:  3084:  3024:  2915:torque 2871:where 2267:where 1340:Adding 1317:where 943:  650:cannot 545:, and 522:, the 75:Right: 4087:is a 3146:with 3043:that 2508:Once 906:with 547:stars 138:Apsis 83:Earth 54:Left: 4451:ISBN 4423:ISBN 4380:ISBN 4166:and 3741:and 3609:and 3063:and 2879:and 2755:and 2519:and 2153:and 1416:Let 1394:and 1077:= 0) 1065:and 1063:= 0) 1049:= 0) 1037:and 1035:= 0) 1005:and 984:and 968:and 959:Let 854:and 577:for 87:Moon 58:mass 4473:at 4351:doi 4015:tot 3274:tot 3239:is 3183:= 2771:). 2117:= − 1621:= − 666:of 613:or 518:In 189:by 4486:: 4449:. 4421:. 4405:; 4349:. 4337:. 4333:. 4171:= 4169:r̂ 3220:. 3179:× 3167:. 3164:dt 3151:= 3052:= 3048:× 2893:− 2505:. 2201:12 2122:21 2115:12 2092:12 2013:21 1984:12 1860:+ 1626:21 1619:12 1590:21 1575:12 1408:. 1372:− 1365:= 1329:21 1322:12 1220:21 1106:12 1079:. 640:. 617:. 541:, 4459:. 4431:. 4388:. 4359:. 4353:: 4345:: 4339:4 4299:n 4261:r 4259:( 4257:F 4243:, 4230:r 4223:) 4220:r 4217:( 4213:F 4209:= 4199:r 4177:r 4175:/ 4173:r 4161:r 4156:r 4134:r 4127:) 4124:r 4121:( 4118:F 4115:= 4112:) 4108:r 4104:( 4100:F 4085:) 4083:r 4081:( 4079:F 4045:2 4041:E 4037:+ 4032:1 4028:E 4024:= 4011:E 4003:) 3999:r 3995:( 3992:U 3985:2 3981:m 3972:+ 3967:2 3962:2 3951:x 3941:2 3937:m 3931:2 3928:1 3923:= 3920:E 3913:2 3909:m 3900:= 3891:2 3887:E 3879:) 3875:r 3871:( 3868:U 3861:1 3857:m 3848:+ 3843:2 3838:1 3827:x 3817:1 3813:m 3807:2 3804:1 3799:= 3796:E 3789:1 3785:m 3776:= 3767:1 3763:E 3747:2 3744:E 3738:1 3735:E 3730:E 3715:r 3707:2 3703:m 3691:= 3686:2 3681:x 3659:r 3651:1 3647:m 3638:= 3633:1 3628:x 3615:2 3612:x 3606:1 3603:x 3588:) 3584:r 3580:( 3577:U 3574:+ 3569:2 3558:r 3545:2 3542:1 3537:= 3534:E 3508:) 3504:r 3500:( 3497:U 3494:+ 3489:2 3478:r 3465:2 3462:1 3457:+ 3452:2 3441:R 3433:) 3428:2 3424:m 3420:+ 3415:1 3411:m 3407:( 3402:2 3399:1 3394:= 3391:) 3387:r 3383:( 3380:U 3377:+ 3372:2 3367:2 3356:x 3346:2 3342:m 3336:2 3333:1 3328:+ 3323:2 3318:1 3307:x 3297:1 3293:m 3287:2 3284:1 3279:= 3270:E 3255:) 3253:r 3251:( 3249:U 3237:) 3235:r 3233:( 3231:F 3217:L 3207:v 3201:r 3193:L 3185:0 3181:F 3177:r 3162:/ 3160:r 3157:d 3153:μ 3149:F 3134:, 3127:F 3119:r 3115:= 3109:t 3106:d 3100:L 3096:d 3087:= 3080:N 3066:w 3060:v 3054:0 3050:w 3046:v 3027:, 3014:r 3000:r 2996:+ 2986:r 2966:r 2959:= 2953:t 2950:d 2944:L 2940:d 2934:= 2930:N 2919:N 2910:L 2904:r 2898:1 2895:r 2891:2 2888:r 2882:r 2873:μ 2857:, 2851:t 2848:d 2842:r 2838:d 2825:r 2821:= 2817:p 2809:r 2805:= 2801:L 2789:L 2780:p 2757:r 2753:R 2739:) 2736:t 2733:( 2729:r 2720:2 2716:m 2712:+ 2707:1 2703:m 2696:1 2692:m 2683:) 2680:t 2677:( 2673:R 2669:= 2666:) 2663:t 2660:( 2655:2 2650:x 2629:) 2626:t 2623:( 2619:r 2610:2 2606:m 2602:+ 2597:1 2593:m 2586:2 2582:m 2576:+ 2573:) 2570:t 2567:( 2563:R 2559:= 2556:) 2553:t 2550:( 2545:1 2540:x 2528:) 2526:t 2524:( 2522:r 2517:) 2515:t 2513:( 2511:R 2485:) 2481:r 2477:( 2473:F 2452:) 2448:r 2444:( 2440:F 2429:) 2427:t 2425:( 2423:r 2406:. 2398:2 2394:m 2390:+ 2385:1 2381:m 2373:2 2369:m 2363:1 2359:m 2352:= 2342:2 2338:m 2334:1 2329:+ 2322:1 2318:m 2314:1 2308:1 2303:= 2255:) 2251:r 2247:( 2243:F 2239:= 2236:) 2231:2 2226:x 2221:, 2216:1 2211:x 2206:( 2196:F 2191:= 2181:r 2159:2 2156:x 2150:1 2147:x 2141:r 2128:r 2119:F 2112:F 2087:F 2081:) 2073:2 2069:m 2065:1 2060:+ 2053:1 2049:m 2045:1 2039:( 2035:= 2031:) 2023:2 2019:m 2008:F 1994:1 1990:m 1979:F 1971:( 1967:= 1962:2 1951:x 1938:1 1927:x 1919:= 1909:r 1887:) 1885:t 1883:( 1881:R 1871:2 1868:v 1865:2 1862:m 1858:1 1855:v 1852:1 1849:m 1831:t 1828:d 1823:R 1820:d 1814:= 1810:v 1789:0 1786:= 1776:R 1750:. 1742:2 1738:m 1734:+ 1729:1 1725:m 1717:2 1706:x 1696:2 1692:m 1688:+ 1683:1 1672:x 1662:1 1658:m 1641:R 1623:F 1616:F 1598:0 1595:= 1585:F 1580:+ 1570:F 1565:= 1555:R 1548:) 1543:2 1539:m 1535:+ 1530:1 1526:m 1522:( 1519:= 1514:2 1503:x 1493:2 1489:m 1485:+ 1480:1 1469:x 1459:1 1455:m 1442:( 1425:R 1406:) 1404:t 1402:( 1400:2 1397:x 1392:) 1390:t 1388:( 1386:1 1383:x 1377:2 1374:x 1370:1 1367:x 1363:r 1352:( 1345:2 1333:x 1326:F 1319:F 1310:) 1308:2 1287:2 1276:x 1266:2 1262:m 1258:= 1255:) 1250:2 1245:x 1240:, 1235:1 1230:x 1225:( 1215:F 1196:) 1194:1 1173:1 1162:x 1152:1 1148:m 1144:= 1141:) 1136:2 1131:x 1126:, 1121:1 1116:x 1111:( 1101:F 1075:t 1073:( 1071:2 1068:v 1061:t 1059:( 1057:1 1054:v 1047:t 1045:( 1043:2 1040:x 1033:t 1031:( 1029:1 1026:x 1021:t 1017:) 1015:t 1013:( 1011:2 1008:x 1003:) 1001:t 999:( 997:1 994:x 989:2 986:m 982:1 979:m 974:2 971:x 965:1 962:x 955:. 938:2 934:m 930:+ 925:1 921:m 917:= 914:M 892:2 887:x 877:1 872:x 867:= 863:r 840:2 835:x 828:M 823:2 819:m 813:+ 808:1 803:x 796:M 791:1 787:m 781:= 777:R 745:) 741:( 723:. 579:n 573:n 507:e 500:t 493:v 375:) 371:( 222:) 213:( 85:– 72:. 27:.

Index

Two-body problem in general relativity
Two-body problem (career)


mass
barycenter
elliptic orbits
binary stars
Pluto–Charon system
Earth
Moon

Orbital mechanics
Orbital elements
Apsis
Argument of periapsis
Eccentricity
Inclination
Mean anomaly
Orbital nodes
Semi-major axis
True anomaly
two-body orbits
Circular orbit
Elliptic orbit
Transfer orbit
Hohmann transfer orbit
Bi-elliptic transfer orbit
Parabolic orbit
Hyperbolic orbit

Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.