guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
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4. 5<br />
4.6<br />
4.7<br />
I+. 8<br />
4.9<br />
I.. 10<br />
I+.11<br />
4.16<br />
4.17<br />
4.18<br />
4.19<br />
Bender, D. F. <strong>and</strong> KcCue, B. A., Conditions for Optimal One-Impulse<br />
Transfer. AAS.J. L;1 (1966) p 163-158<br />
Strahly, I..*. H.., Utilizing the Phasing Technique in Rendezvous.<br />
ARS Preprint 61-2295 Space Flight Report, New Yor!c (Ott 1961)<br />
Bendcr D. F., Rendezvous Possibilitie s with the Impulse of Optimum<br />
Two-Impulse Transfer.- Adv. in the Astronautical Science Vol. 16<br />
Part 1. p 271-291. LSpace Rendezvous Rescue <strong>and</strong> Recovery Edwards AFB<br />
(Sept. 1963)J<br />
Bender, D. F. , @imum Codanar Impulsive Transfer between Elliptic<br />
---<br />
Orbits. Aero Space Eng. 21 No. 10 (Oct. 1962) p 44-52<br />
Goldstein, A. A., <strong>and</strong> Greene, A. H., Johnson, A. T., <strong>and</strong> Seidman, T. I.,<br />
_ Fuel O@,imizaticn ___- in Orbital Rendezvous.<br />
-.--- AIAA Preprint 63-354<br />
(Guidance <strong>and</strong> Control Conference, Cambridge, Wass., Aug. 1963)<br />
Bryson, A. E. Jr., -____ Linear __--._- Feedback _______-__ Solutions for Minimum Effort<br />
- Interceptiog, ---<br />
Rcnde_z_vous, <strong>and</strong> Soft L<strong>and</strong>s. AIA;\J 3 (1965)<br />
p 1542-1544<br />
Paicwonsky, B. H. <strong>and</strong> :!oodrow. _---- A Studyf - Time Optimal .------- Rendezvous<br />
-- in Three ---~ Dimansions (Vol. 1). TDR No. AFFDL-TR-65-20 >/right Patterson<br />
;iFB Jan 1965 (AD 624218)<br />
Iu,cIntyre, J. 1.. , xhg_-Pcntxa.gin Ilaximum Principle, NAA/SID 65-1200-7<br />
-<br />
(IC2.y 1764)<br />
rq’p, ii. E. , Pnntr~+n l.laxirnum Principle. Ch(apter 7 of Optimization<br />
Tochn'outis, Ed. Lertman, Academic :.;icss (1962)<br />
I.-:cc!lc !;. A ., -L--.-.1;.-_-..--:<br />
~unsili~earizatlo~ -,-- Detcrrxination -.~ -.I___ of $timum Finitg-Thrust<br />
--_-- i?rbitil Trnnsf:rs, 210 66-1278 (to be published in AIiiA Journal)<br />
li<strong>and</strong>elsm.7n, ?4. , Optim:11 Free-Space -- F,,, ;~ed-Thrust ---.-.- Trqjectorics Usin?<br />
Impulsive ___--- Trajectories _ _-I_--.--. as Z.tnrt5.n:: Iteratives, AIAA Journal 4 (1966)<br />
p 1077-1082<br />
Gunckel, T. L., Near Earth Guidance Techniques. UCLA Short Course on<br />
Space Navigations <strong>and</strong> Guidance. (Sept. 1966)<br />
Kelbourne, I;. G. <strong>and</strong> Sauer, G. G., Optimum Interplanetary Rendezvous<br />
TraJJcctories _,__.-- - -- with -.- Power Limited<br />
October 1962<br />
Vehicles, JPL TK No. 32-226. (Rev. 1)<br />
Gobetz, F. :1., A Linear Theory of Optimum Lo:+Thrust Rendezvous<br />
Trajectories. AASJ 3 (196';) p 69-76<br />
-<br />
Soule P . ::.<br />
Rendeivous.<br />
, <strong>and</strong> iiidd, A. T., Terminal Maneuvers for Satellite Ascent<br />
Presented at LAS/ARS Joint Meeting, Los Angeles, June 1961<br />
89
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