Fundamentals of astrodynamics and applications 4th Edition (2013)

Recommendations

Info

Common Two-body EquationsSpecific Angular Momentumh = r × vh = mp = rv COS( f fpa ) = r 2 ṅ = r a v a = r p v pSpecific Mechanical Energyvy2 m m= ----- – --- = –-----2 r 2aOrbital PeriodEccentricity VectorRadius=2p a3 -----mv 2 m– --- r – ( r ⋅ v)v r e = -----------------------------------------------mpr = -------------------------------1 + e COS( n)Radial RateSemi-parameter. rṅ e SIN( n)r = -------------------------------1 + e COS( n)nan· = -------- 2r 2 1 – e 2ph= -----2mSemi-major axisa m------- 2 13 / m= = ----- 2p 3n 2continued on next page
Circle Ellipse Parabola Hyperbola14.03.05.010.0v0.0F, F′r0.0bpF′ Fr ar pvr0.0F′ Fvrp0.0pFvr prF′cr p−aa–3.0–3.0Eccentric Anomalya, r, p0.0 3.0 ERUndefined–5.0–9.00.0 4.0 ER–10.0–12.0M – E n + eSIN( E n )E n + 1 = E + ----------------------------------------------n 1 – eCOS( E n )0.0 8.0–14.0–10.00.0 10.0M–eSINH( H n ) + H nH n+1 = H n + ---------------------------------------------------e COSH( H n )–1SIN( E)COS( E)SIN( n) 1 – e= -----------------------------------21 + e COS( n)e + COS( n)= ------------------------------1 + e COS( n)B =nTAN -- 2SINH( H)COSH( H)SIN( n) e 2 – 1= -----------------------------------1 + e COS( n)e + COS( n)= ------------------------------1 + e COS( n)True AnomalyUndefinedSIN( n)COS( n)SIN( E) 1 – e= -----------------------------------21 – eCOS( E)COS( E)– e= ------------------------------1 – eCOS( E)pBSIN( n)= ------rCOS( n)p–r= ----------rSIN( n)COS( n)– SINH( H) e 2 – 1= -------------------------------------------1 – eCOSH( H)COSH( H)– e= ----------------------------------1 – eCOSH( H)Flight Path Anglef fpa = 0°SIN( f fpa )COS( f fpa )eSIN( E)= -------------------------------------------1 – e 2 COS 2 ( E)=-----------------------------------1 – e 21 – e 2 COS 2 ( E)f parabolicn= --2SIN( f fpa )COS( f fpa )– e SINH( H)= -------------------------------------------=e 2 COSH 2 ( H) – 1e 2 – 1-----------------------------------------e 2 COSH 2 ( H)– 1
Page 5: CircleEllipse Parabola HyperbolaEqu
Page 9 and 10: FUNDAMENTALS OF ASTRODYNAMICS AND A
Page 11 and 12: Fundamentals of Astrodynamicsand Ap
Page 13: To God from whom all blessings and
Page 16 and 17: viii3.3 Coordinate Systems 1453.3.1
Page 18 and 19: x7.4.2 Range-only Processing 4527.5
Page 20 and 21: xii11.2.2 Mission Planning 85211.3
Page 22 and 23: xivAlgorithm SummaryAlgorithm 1 Fin
Page 24 and 25: xviForwardAt Microcosm, when an ast
Page 26 and 27: xviiineed,” only to find that you
Page 28 and 29: xxAcknowledgmentsI credit numerous
Page 30 and 31: xxiiald Dichmann, John Douglass, Te
Page 32 and 33: 2 EQUATIONS OF MOTION 1.1one, . . .
Page 34 and 35: 4 EQUATIONS OF MOTION 1.1modern tec
Page 36 and 37: 6 EQUATIONS OF MOTION 1.1occurred a
Page 38 and 39: 8 EQUATIONS OF MOTION 1.1numbers an
Page 40 and 41: 10 EQUATIONS OF MOTION 1.1Finally,
Page 42 and 43: 12 EQUATIONS OF MOTION 1.21.1.5 Oth
Page 44 and 45: 14 EQUATIONS OF MOTION 1.2Directrix
Page 46 and 47: 16 EQUATIONS OF MOTION 1.219134vre
Page 48 and 49: 18 EQUATIONS OF MOTION 1.214.0e = 5
Page 50 and 51: 20 EQUATIONS OF MOTION 1.3from apoa
Page 52 and 53:
22 EQUATIONS OF MOTION 1.3r K sat=
Page 54 and 55:
24 EQUATIONS OF MOTION 1.3..mr× r
Page 56 and 57:
26 EQUATIONS OF MOTION 1.3.v ⋅ v
Page 58 and 59:
28 EQUATIONS OF MOTION 1.3m--- ( r
Page 60 and 61:
30 EQUATIONS OF MOTION 1.3The perio
Page 62 and 63:
32 EQUATIONS OF MOTION 1.3(1) Using
Page 64 and 65:
34 EQUATIONS OF MOTION 1.4EarthThir
Page 66 and 67:
36 EQUATIONS OF MOTION 1.4geometry.
Page 68 and 69:
38 EQUATIONS OF MOTION 1.4ni = 1.m
Page 70 and 71:
40 EQUATIONS OF MOTION 1.4n1 2 1 my
Page 72 and 73:
42 KEPLER’S EQUATION AND KEPLER
Page 74 and 75:
Page 76 and 77:
Page 78 and 79:
Page 80 and 81:
Page 82 and 83:
Page 84 and 85:
Page 86 and 87:
Page 88 and 89:
Page 90 and 91:
Page 92 and 93:
Page 94 and 95:
Page 96 and 97:
Page 98 and 99:
Page 100 and 101:
Page 102 and 103:
Page 104 and 105:
Page 106 and 107:
Page 108 and 109:
Page 110 and 111:
Page 112 and 113:
Page 114 and 115:
Page 116 and 117:
Page 118 and 119:
Page 120 and 121:
Page 122 and 123:
Page 124 and 125:
Page 126 and 127:
Page 128 and 129:
Page 130 and 131:
Page 132 and 133:
Page 134 and 135:
Page 136 and 137:
Page 138 and 139:
Page 140 and 141:
Page 142 and 143:
Page 144 and 145:
Page 146 and 147:
Page 148 and 149:
Page 150 and 151:
Page 152 and 153:
Page 154 and 155:
Page 156 and 157:
Page 158 and 159:
Page 160 and 161:
130 COORDINATE AND TIME SYSTEMS 3.1
Page 162 and 163:
Page 164 and 165:
Page 166 and 167:
Page 168 and 169:
Page 170 and 171:
Page 172 and 173:
Page 174 and 175:
Page 176 and 177:
Page 178 and 179:
Page 180 and 181:
Page 182 and 183:
Page 184 and 185:
Page 186 and 187:
Page 188 and 189:
Page 190 and 191:
Page 192 and 193:
Page 194 and 195:
Page 196 and 197:
Page 198 and 199:
Page 200 and 201:
Page 202 and 203:
Page 204 and 205:
Page 206 and 207:
Page 208 and 209:
Page 210 and 211:
Page 212 and 213:
Page 214 and 215:
Page 216 and 217:
Page 218 and 219:
Page 220 and 221:
Page 222 and 223:
Page 224 and 225:
Page 226 and 227:
Page 228 and 229:
Page 230 and 231:
Page 232 and 233:
Page 234 and 235:
Page 236 and 237:
Page 238 and 239:
Page 240 and 241:
Page 242 and 243:
Page 244 and 245:
Page 246 and 247:
Page 248 and 249:
Page 250 and 251:
Page 252 and 253:
Page 254 and 255:
Page 256 and 257:
Page 258 and 259:
Page 260 and 261:
Page 262 and 263:
Page 264 and 265:
Page 266 and 267:
Page 268 and 269:
Page 270 and 271:
Page 272 and 273:
242 OBSERVATIONS 4.2numerals, effec
Page 274 and 275:
244 OBSERVATIONS 4.2t s-rect s-tran
Page 276 and 277:
246 OBSERVATIONS 4.2SEZObserved Pla
Page 278 and 279:
248 OBSERVATIONS 4.24.2.3 Types of
Page 280 and 281:
250 OBSERVATIONS 4.3egories: dedica
Page 282 and 283:
252 OBSERVATIONS 4.3which have corn
Page 284 and 285:
254 OBSERVATIONS 4.4TABLE 4-3. Phys
Page 286 and 287:
256 OBSERVATIONS 4.4ClearCavalierSo
Page 288 and 289:
258 OBSERVATIONS 4.4ṙ COS( d)COS(
Page 290 and 291:
260 OBSERVATIONS 4.4fixed orientati
Page 292 and 293:
262 OBSERVATIONS 4.4.. - ṙ COS( e
Page 294 and 295:
264 OBSERVATIONS 4.4Notice several
Page 296 and 297:
266 OBSERVATIONS 4.4RAZEL is simply
Page 298 and 299:
268 OBSERVATIONS 4.4SIN( b)SIN( LHA
Page 300 and 301:
270 OBSERVATIONS 4.4This equation y
Page 302 and 303:
272 OBSERVATIONS 4.420181614Inclina
Page 304 and 305:
274 OBSERVATIONS 4.4d = -20°49'24.
Page 306 and 307:
276 OBSERVATIONS 4.4Problems1. You
Page 308 and 309:
278 CELESTIAL PHENOMENA 5.1K^eZ^Ecl
Page 310 and 311:
280 CELESTIAL PHENOMENA 5.1M L = 35
Page 312 and 313:
282 CELESTIAL PHENOMENA 5.1SunLunar
Page 314 and 315:
284 CELESTIAL PHENOMENA 5.1TAN( a L
Page 316 and 317:
286 CELESTIAL PHENOMENA 5.25.2.1 Ap
Page 318 and 319:
288 CELESTIAL PHENOMENA 5.2ALGORITH
Page 320 and 321:
290 CELESTIAL PHENOMENA 5.25.2.2 Ap
Page 322 and 323:
292 CELESTIAL PHENOMENA 5.2JD temp
Page 324 and 325:
294 CELESTIAL PHENOMENA 5.3Set GHA
Page 326 and 327:
296 CELESTIAL PHENOMENA 5.3e = 0.04
Page 328 and 329:
298 CELESTIAL PHENOMENA 5.32-6 3Q =
Page 330 and 331:
300 CELESTIAL PHENOMENA 5.3minutes
Page 332 and 333:
302 CELESTIAL PHENOMENA 5.3SAT hori
Page 334 and 335:
304 CELESTIAL PHENOMENA 5.3Unfortun
Page 336 and 337:
306 CELESTIAL PHENOMENA 5.3lite has
Page 338 and 339:
308 CELESTIAL PHENOMENA 5.3c( t min
Page 340 and 341:
310 CELESTIAL PHENOMENA 5.3L 1 = l
Page 342 and 343:
312 CELESTIAL PHENOMENA 5.3the sola
Page 344 and 345:
314 CELESTIAL PHENOMENA 5.3a6378SIN
Page 346 and 347:
316 CELESTIAL PHENOMENA 5.3Problems
Page 348 and 349:
318 ORBITAL MANEUVERING 6.2After so
Page 350 and 351:
320 ORBITAL MANEUVERING 6.3The subs
Page 352 and 353:
322 ORBITAL MANEUVERING 6.3v transb
Page 354 and 355:
324 ORBITAL MANEUVERING 6.3Trans 1b
Page 356 and 357:
326 ORBITAL MANEUVERING 6.3ALGORITH
Page 358 and 359:
328 ORBITAL MANEUVERING 6.32mm21 (
Page 360 and 361:
330 ORBITAL MANEUVERING 6.3R* = 15.
Page 362 and 363:
332 ORBITAL MANEUVERING 6.3Substitu
Page 364 and 365:
334 ORBITAL MANEUVERING 6.3COS( E)=
Page 366 and 367:
336 ORBITAL MANEUVERING 6.3TABLE 6-
Page 368 and 369:
338 ORBITAL MANEUVERING 6.4close to
Page 370 and 371:
340 ORBITAL MANEUVERING 6.480Latitu
Page 372 and 373:
342 ORBITAL MANEUVERING 6.46.4.2 In
Page 374 and 375:
344 ORBITAL MANEUVERING 6.4ALGORITH
Page 376 and 377:
346 ORBITAL MANEUVERING 6.4K^v fina
Page 378 and 379:
348 ORBITAL MANEUVERING 6.46.4.4 Ch
Page 380 and 381:
350 ORBITAL MANEUVERING 6.5Up to th
Page 382 and 383:
352 ORBITAL MANEUVERING 6.5change t
Page 384 and 385:
354 ORBITAL MANEUVERING 6.5TABLE 6-
Page 386 and 387:
356 ORBITAL MANEUVERING 6.5COS( g)=
Page 388 and 389:
358 ORBITAL MANEUVERING 6.6Sec. 7.6
Page 390 and 391:
360 ORBITAL MANEUVERING 6.6tions. F
Page 392 and 393:
362 ORBITAL MANEUVERING 6.6c = a L
Page 394 and 395:
364 ORBITAL MANEUVERING 6.6Δv= 2(
Page 396 and 397:
366 ORBITAL MANEUVERING 6.6solution
Page 398 and 399:
368 ORBITAL MANEUVERING 6.6node wit
Page 400 and 401:
370 ORBITAL MANEUVERING 6.6^J^KInte
Page 402 and 403:
372 ORBITAL MANEUVERING 6.7or physi
Page 404 and 405:
374 ORBITAL MANEUVERING 6.7For gene
Page 406 and 407:
376 ORBITAL MANEUVERING 6.7Because
Page 408 and 409:
378 ORBITAL MANEUVERING 6.710Accumu
Page 410 and 411:
380 ORBITAL MANEUVERING 6.7Then, fi
Page 412 and 413:
382 ORBITAL MANEUVERING 6.7c(v p )
Page 414 and 415:
384 ORBITAL MANEUVERING 6.7Now find
Page 416 and 417:
386 ORBITAL MANEUVERING 6.7Numerica
Page 418 and 419:
388 ORBITAL MANEUVERING 6.8Δv acc
Page 420 and 421:
390 ORBITAL MANEUVERING 6.8.. mr= -
Page 422 and 423:
392 ORBITAL MANEUVERING 6.8..r I=..
Page 424 and 425:
394 ORBITAL MANEUVERING 6.8Take the
Page 426 and 427:
396 ORBITAL MANEUVERING 6.8yt ()=..
Page 428 and 429:
398 ORBITAL MANEUVERING 6.8. .ẋ()
Page 430 and 431:
400 ORBITAL MANEUVERING 6.8Now, rew
Page 432 and 433:
402 ORBITAL MANEUVERING 6.8150x(m)1
Page 434 and 435:
404 ORBITAL MANEUVERING 6.8velocity
Page 436 and 437:
406 ORBITAL MANEUVERING 6.8x(m)2000
Page 438 and 439:
408 ORBITAL MANEUVERING 6.8Intercep
Page 440 and 441:
410 ORBITAL MANEUVERING 6.8. - 2qx
Page 442 and 443:
412 ORBITAL MANEUVERING 6.8presente
Page 444 and 445:
414 ORBITAL MANEUVERING 6.8point 2
Page 446 and 447:
416 ORBITAL MANEUVERING 6.8z= -----
Page 448 and 449:
418 ORBITAL MANEUVERING 6.810.000y
Page 450 and 451:
420 ORBITAL MANEUVERING 6.8Problems
Page 452 and 453:
422 ORBITAL MANEUVERING 6.8
Page 454 and 455:
424 INITIAL ORBIT DETERMINATION 7.1
Page 456 and 457:
Page 458 and 459:
Page 460 and 461:
Page 462 and 463:
Page 464 and 465:
Page 466 and 467:
Page 468 and 469:
Page 470 and 471:
Page 472 and 473:
Page 474 and 475:
Page 476 and 477:
Page 478 and 479:
Page 480 and 481:
Page 482 and 483:
Page 484 and 485:
Page 486 and 487:
Page 488 and 489:
Page 490 and 491:
Page 492 and 493:
Page 494 and 495:
Page 496 and 497:
Page 498 and 499:
Page 500 and 501:
Page 502 and 503:
Page 504 and 505:
Page 506 and 507:
Page 508 and 509:
Page 510 and 511:
Page 512 and 513:
Page 514 and 515:
Page 516 and 517:
Page 518 and 519:
Page 520 and 521:
Page 522 and 523:
Page 524 and 525:
Page 526 and 527:
Page 528 and 529:
Page 530 and 531:
Page 532 and 533:
Page 534 and 535:
Page 536 and 537:
Page 538 and 539:
Page 540 and 541:
Page 542 and 543:
Page 544 and 545:
Page 546 and 547:
Page 548 and 549:
518 SPECIAL PERTURBATION TECHNIQUES
Page 550 and 551:
Page 552 and 553:
Page 554 and 555:
Page 556 and 557:
Page 558 and 559:
Page 560 and 561:
Page 562 and 563:
Page 564 and 565:
Page 566 and 567:
Page 568 and 569:
Page 570 and 571:
Page 572 and 573:
Page 574 and 575:
Page 576 and 577:
Page 578 and 579:
Page 580 and 581:
Page 582 and 583:
Page 584 and 585:
Page 586 and 587:
Page 588 and 589:
Page 590 and 591:
Page 592 and 593:
Page 594 and 595:
Page 596 and 597:
Page 598 and 599:
Page 600 and 601:
Page 602 and 603:
Page 604 and 605:
Page 606 and 607:
Page 608 and 609:
Page 610 and 611:
Page 612 and 613:
Page 614 and 615:
Page 616 and 617:
Page 618 and 619:
Page 620 and 621:
Page 622 and 623:
Page 624 and 625:
Page 626 and 627:
Page 628 and 629:
Page 630 and 631:
Page 632 and 633:
Page 634 and 635:
Page 636 and 637:
Page 638 and 639:
Page 640 and 641:
610 GENERAL PERTURBATION TECHNIQUES
Page 642 and 643:
Page 644 and 645:
Page 646 and 647:
Page 648 and 649:
Page 650 and 651:
Page 652 and 653:
Page 654 and 655:
Page 656 and 657:
Page 658 and 659:
Page 660 and 661:
Page 662 and 663:
Page 664 and 665:
Page 666 and 667:
Page 668 and 669:
Page 670 and 671:
Page 672 and 673:
Page 674 and 675:
Page 676 and 677:
Page 678 and 679:
Page 680 and 681:
Page 682 and 683:
Page 684 and 685:
Page 686 and 687:
Page 688 and 689:
Page 690 and 691:
Page 692 and 693:
Page 694 and 695:
Page 696 and 697:
Page 698 and 699:
Page 700 and 701:
Page 702 and 703:
Page 704 and 705:
Page 706 and 707:
Page 708 and 709:
Page 710 and 711:
Page 712 and 713:
Page 714 and 715:
Page 716 and 717:
Page 718 and 719:
Page 720 and 721:
Page 722 and 723:
Page 724 and 725:
Page 726 and 727:
Page 728 and 729:
Page 730 and 731:
Page 732 and 733:
Page 734 and 735:
Page 736 and 737:
Page 738 and 739:
Page 740 and 741:
Page 742 and 743:
Page 744 and 745:
Page 746 and 747:
Page 748 and 749:
Page 750 and 751:
Page 752 and 753:
Page 754 and 755:
Page 756 and 757:
Page 758 and 759:
Page 760 and 761:
Page 762 and 763:
732 ORBIT DETERMINATION AND ESTIMAT
Page 764 and 765:
Page 766 and 767:
Page 768 and 769:
Page 770 and 771:
Page 772 and 773:
Page 774 and 775:
Page 776 and 777:
Page 778 and 779:
Page 780 and 781:
Page 782 and 783:
Page 784 and 785:
Page 786 and 787:
Page 788 and 789:
Page 790 and 791:
Page 792 and 793:
Page 794 and 795:
Page 796 and 797:
Page 798 and 799:
Page 800 and 801:
Page 802 and 803:
Page 804 and 805:
Page 806 and 807:
Page 808 and 809:
Page 810 and 811:
Page 812 and 813:
Page 814 and 815:
Page 816 and 817:
Page 818 and 819:
Page 820 and 821:
Page 822 and 823:
Page 824 and 825:
Page 826 and 827:
Page 828 and 829:
Page 830 and 831:
Page 832 and 833:
Page 834 and 835:
Page 836 and 837:
Page 838 and 839:
Page 840 and 841:
Page 842 and 843:
Page 844 and 845:
Page 846 and 847:
Page 848 and 849:
Page 850 and 851:
Page 852 and 853:
Page 854 and 855:
Page 856 and 857:
Page 858 and 859:
Page 860 and 861:
Page 862 and 863:
Page 864 and 865:
Page 866 and 867:
Page 868 and 869:
838 MISSION ANALYSIS 11.1developing
Page 870 and 871:
840 MISSION ANALYSIS 11.1Today, the
Page 872 and 873:
842 MISSION ANALYSIS 11.1tasked to
Page 874 and 875:
844 MISSION ANALYSIS 11.1Upgrades s
Page 876 and 877:
846 MISSION ANALYSIS 11.2The eccent
Page 878 and 879:
848 MISSION ANALYSIS 11.22000100000
Page 880 and 881:
850 MISSION ANALYSIS 11.2TABLE 11-2
Page 882 and 883:
852 MISSION ANALYSIS 11.2An importa
Page 884 and 885:
854 MISSION ANALYSIS 11.3applies to
Page 886 and 887:
856 MISSION ANALYSIS 11.3eral speci
Page 888 and 889:
858 MISSION ANALYSIS 11.3r horizong
Page 890 and 891:
860 MISSION ANALYSIS 11.3Use these
Page 892 and 893:
862 MISSION ANALYSIS 11.4SIN 2 ( L)
Page 894 and 895:
864 MISSION ANALYSIS 11.4^KSun1200A
Page 896 and 897:
866 MISSION ANALYSIS 11.4where usin
Page 898 and 899:
868 MISSION ANALYSIS 11.4drift to t
Page 900 and 901:
870 MISSION ANALYSIS 11.4ascending
Page 902 and 903:
872 MISSION ANALYSIS 11.4Rev 17Rev
Page 904 and 905:
874 MISSION ANALYSIS 11.4motion. Fo
Page 906 and 907:
876 MISSION ANALYSIS 11.4Δλ rev=
Page 908 and 909:
878 MISSION ANALYSIS 11.4If we take
Page 910 and 911:
880 MISSION ANALYSIS 11.411.4.3 Min
Page 912 and 913:
882 MISSION ANALYSIS 11.4the most e
Page 914 and 915:
884 MISSION ANALYSIS 11.4∂ 2 r---
Page 916 and 917:
886 MISSION ANALYSIS 11.4dq-------d
Page 918 and 919:
888 MISSION ANALYSIS 11.4tories for
Page 920 and 921:
890 MISSION ANALYSIS 11.4The mean m
Page 922 and 923:
892 MISSION ANALYSIS 11.4When you d
Page 924 and 925:
894 MISSION ANALYSIS 11.42π-----Q1
Page 926 and 927:
896 MISSION ANALYSIS 11.5Longitude
Page 928 and 929:
898 MISSION ANALYSIS 11.5the precis
Page 930 and 931:
900 MISSION ANALYSIS 11.5•••
Page 932 and 933:
902 MISSION ANALYSIS 11.5Pseudorang
Page 934 and 935:
904 MISSION ANALYSIS 11.5an integer
Page 936 and 937:
906 MISSION ANALYSIS 11.5of code ps
Page 938 and 939:
908 MISSION ANALYSIS 11.6known rece
Page 940 and 941:
910 MISSION ANALYSIS 11.6the interv
Page 942 and 943:
912 MISSION ANALYSIS 11.6DAT, x p ,
Page 944 and 945:
914 MISSION ANALYSIS 11.6TABLE 11-4
Page 946 and 947:
916 MISSION ANALYSIS 11.690Elevatio
Page 948 and 949:
918 MISSION ANALYSIS 11.6f range ()
Page 950 and 951:
920 MISSION ANALYSIS 11.7Satellite
Page 952 and 953:
922 MISSION ANALYSIS 11.7For this d
Page 954 and 955:
924 MISSION ANALYSIS 11.7Woodburn e
Page 956 and 957:
926 MISSION ANALYSIS 11.7t close (
Page 958 and 959:
928 MISSION ANALYSIS 11.7straight a
Page 960 and 961:
930 MISSION ANALYSIS 11.7for the P
Page 962 and 963:
932 MISSION ANALYSIS 11.7riance ell
Page 964 and 965:
934 MISSION ANALYSIS 11.7If the cal
Page 966 and 967:
936 MISSION ANALYSIS 11.7d close=P2
Page 968 and 969:
938 MISSION ANALYSIS 11.7the correc
Page 970 and 971:
940 MISSION ANALYSIS 11.7
Page 972 and 973:
942 INTERPLANETARY MISSION ANALYSIS
Page 974 and 975:
Page 976 and 977:
Page 978 and 979:
Page 980 and 981:
Page 982 and 983:
Page 984 and 985:
Page 986 and 987:
Page 988 and 989:
Page 990 and 991:
Page 992 and 993:
Page 994 and 995:
Page 996 and 997:
Page 998 and 999:
Page 1000 and 1001:
Page 1002 and 1003:
Page 1004 and 1005:
Page 1006 and 1007:
Page 1008 and 1009:
Page 1010 and 1011:
Page 1012 and 1013:
Page 1014 and 1015:
Page 1016 and 1017:
Page 1018 and 1019:
Page 1020 and 1021:
990 APPENDIX Aaaa iâ iacc iSemimaj
Page 1022 and 1023:
992 APPENDIX Att acct dirftt mt pt
Page 1024 and 1025:
994 APPENDIX AG mpG pHHHH dH pq'Ecc
Page 1026 and 1027:
996 APPENDIX AbbAzimuth, measured p
Page 1028 and 1029:
998 APPENDIX At iDelta time between
Page 1030 and 1031:
Dictionary of Symbols
Page 1032 and 1033:
1002 APPENDIX B180.0° rLHA L-----
Page 1034 and 1035:
1004 APPENDIX BB.1.3Evaluating Dens
Page 1036 and 1037:
1006 APPENDIX Bf=35 4 R2-----------
Page 1038 and 1039:
1008 APPENDIX BWe also need the par
Page 1040 and 1041:
1010 APPENDIX B( Δlog 10 r) He0.65
Page 1042 and 1043:
1012 APPENDIX BTime lags are used f
Page 1044 and 1045:
1014 APPENDIX BTABLE B-7. Russian D
Page 1046 and 1047:
1016 APPENDIX BTABLE B-9. Russian D
Page 1048 and 1049:
1018 APPENDIX Cerf( z)=z------2e t2
Page 1050 and 1051:
1020 APPENDIX Cy= C T X z = A T X +
Page 1052 and 1053:
1022 APPENDIX CSIN( a+b)= SIN( a)CO
Page 1054 and 1055:
1024 APPENDIX CFor the right triang
Page 1056 and 1057:
1026 APPENDIX CcACbBaFigure C-4.Obl
Page 1058 and 1059:
1028 APPENDIX CNow find the constan
Page 1060 and 1061:
1030 APPENDIX Ca=1-- 3( P32 - 4R) -
Page 1062 and 1063:
1032 APPENDIX Cfunctions, for which
Page 1064 and 1065:
1034 APPENDIX Cfirst equation of Eq
Page 1066 and 1067:
1036 APPENDIX CIF a c0 < 0.0 and MA
Page 1068 and 1069:
1038 APPENDIX Cno such roots exist
Page 1070 and 1071:
1040 APPENDIX DTABLE D-2. Selected
Page 1072 and 1073:
1042 APPENDIX DTABLE D-4. Mean Plan
Page 1074 and 1075:
1044 APPENDIX DTABLE D-7. Largest I
Page 1076 and 1077:
1046 APPENDIX DD.4 Planetary Epheme
Page 1078 and 1079:
1048 APPENDIX Dq˜2= 173.005 159°
Page 1080 and 1081:
1050 APPENDIX DNeptunei23= 1.769 95
Page 1082 and 1083:
1052 APPENDIX Dannual period, AnnPe
Page 1084 and 1085:
1054 APPENDIX DCurrent Yearyyyy.vm(
Page 1086 and 1087:
1056 APPENDIX DObservational Data:R
Page 1088 and 1089:
1058 APPENDIX D| CROSS CROSS produc
Page 1090 and 1091:
1060 APPENDIX DTABLE D-10. Orbit De
Page 1092 and 1093:
1062 REFERENCESAllan, R. R., and G.
Page 1094 and 1095:
1064 REFERENCESBrewer, J.A., and D.
Page 1096 and 1097:
1066 REFERENCESChilulli, Roy M. 199
Page 1098 and 1099:
1068 REFERENCESEscobal, Pedro R. [1
Page 1100 and 1101:
1070 REFERENCES———. 1997. A N
Page 1102 and 1103:
1072 REFERENCESHoots, Felix R., Lin
Page 1104 and 1105:
1074 REFERENCESKnowles, Stephen H.
Page 1106 and 1107:
1076 REFERENCESMcCarthy, Dennis. 19
Page 1108 and 1109:
1078 REFERENCESNostrand, Philip M.
Page 1110 and 1111:
1080 REFERENCESSchumacher, Paul W.,
Page 1112 and 1113:
1082 REFERENCESSutton, Eric K., Jef
Page 1114 and 1115:
1084 REFERENCESVallado, David A., a
Page 1116 and 1117:
1086 REFERENCESZarchan, Paul. 1994.
Page 1118 and 1119:
1088 INDEXRussian GOST, 571Soviet C
Page 1120 and 1121:
1090 INDEXDay of the yearderiving,
Page 1122 and 1123:
1092 INDEXEquinoctial elements, 108
Page 1124 and 1125:
1094 INDEXdetermining period, 122ec
Page 1126 and 1127:
1096 INDEXLAGEOS See Laser Geodynam
Page 1128 and 1129:
1098 INDEXNewton, Isaac 41, 129, 31
Page 1130 and 1131:
1100 INDEXPerturbation effectscentr
Page 1132 and 1133:
1102 INDEX853Rectification point, 5
Page 1134 and 1135:
1104 INDEXSpecific force, 522Specif
Page 1136 and 1137:
1106 INDEXVariational equations 803
Page 1138:
Constants & ConversionsWe can use t
show all

Fundamentals of astrodynamics and applications 4th Edition (2013)

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?