4. 5 4.6 4.7 I+. 8 4.9 I.. 10 I+.11 4.16 4.17 4.18 4.19 Bender, D. F. <strong>and</strong> KcCue, B. A., Conditions for Optimal One-Impulse Transfer. AAS.J. L;1 (1966) p 163-158 Strahly, I..*. H.., Utilizing the Phasing Technique in Rendezvous. ARS Preprint 61-2295 Space Flight Report, New Yor!c (Ott 1961) Bendcr D. F., Rendezvous Possibilitie s with the Impulse of Optimum Two-Impulse Transfer.- Adv. in the Astronautical Science Vol. 16 Part 1. p 271-291. LSpace Rendezvous Rescue <strong>and</strong> Recovery Edwards AFB (Sept. 1963)J Bender, D. F. , @imum Codanar Impulsive Transfer between Elliptic --- Orbits. Aero Space Eng. 21 No. 10 (Oct. 1962) p 44-52 Goldstein, A. A., <strong>and</strong> Greene, A. H., Johnson, A. T., <strong>and</strong> Seidman, T. I., _ Fuel O@,imizaticn ___- in Orbital Rendezvous. -.--- AIAA Preprint 63-354 (Guidance <strong>and</strong> Control Conference, Cambridge, Wass., Aug. 1963) Bryson, A. E. Jr., -____ Linear __--._- Feedback _______-__ Solutions for Minimum Effort - Interceptiog, --- Rcnde_z_vous, <strong>and</strong> Soft L<strong>and</strong>s. AIA;\J 3 (1965) p 1542-1544 Paicwonsky, B. H. <strong>and</strong> :!oodrow. _---- A Studyf - Time Optimal .------- Rendezvous -- in Three ---~ Dimansions (Vol. 1). TDR No. AFFDL-TR-65-20 >/right Patterson ;iFB Jan 1965 (AD 624218) Iu,cIntyre, J. 1.. , xhg_-Pcntxa.gin Ilaximum Principle, NAA/SID 65-1200-7 - (IC2.y 1764) rq’p, ii. E. , Pnntr~+n l.laxirnum Principle. Ch(apter 7 of Optimization Tochn'outis, Ed. Lertman, Academic :.;icss (1962) I.-:cc!lc !;. A ., -L--.-.1;.-_-..--: ~unsili~earizatlo~ -,-- Detcrrxination -.~ -.I___ of $timum Finitg-Thrust --_-- i?rbitil Trnnsf:rs, 210 66-1278 (to be published in AIiiA Journal) li<strong>and</strong>elsm.7n, ?4. , Optim:11 Free-Space -- F,,, ;~ed-Thrust ---.-.- Trqjectorics Usin? Impulsive ___--- Trajectories _ _-I_--.--. as Z.tnrt5.n:: Iteratives, AIAA Journal 4 (1966) p 1077-1082 Gunckel, T. L., Near Earth Guidance Techniques. UCLA Short Course on Space Navigations <strong>and</strong> Guidance. (Sept. 1966) Kelbourne, I;. G. <strong>and</strong> Sauer, G. G., Optimum Interplanetary Rendezvous TraJJcctories _,__.-- - -- with -.- Power Limited October 1962 Vehicles, JPL TK No. 32-226. (Rev. 1) Gobetz, F. :1., A Linear Theory of Optimum Lo:+Thrust Rendezvous Trajectories. AASJ 3 (196';) p 69-76 - Soule P . ::. Rendeivous. , <strong>and</strong> iiidd, A. T., Terminal Maneuvers for Satellite Ascent Presented at LAS/ARS Joint Meeting, Los Angeles, June 1961 89
4.20 Bakalyar, G., Continuous Thrust Rendezvous Transfers&roximately Mars mtremized, The Martin Company ~-61-22 (August 1961) 4.21 Eskridge, C. D., et. al., An Adaptive Guidance Scheme for Orbital Rendezvous, Paper 43, AAS Southeastern Symposium on Missiles & Aerospace Vehicles Sciences. Huntsville Alabama (December 1966) 4.22 Miller, B. J. <strong>and</strong> Abbott, A. S., Observation Theory <strong>and</strong> Sensors, NAA-SID 65-1200-2 (Dee 1965) 4.23 Townsend, G. E., et. al., Boost Guidance squations, NAA-SID 65-1200-8 (Kay 1966) 4.24 Robbins, H. M., An Analytical Study of the Impulsive Approximation, AIAA Journal,& (1966) p 1417-1423 90 NASA-Langley, 1968 - 30 CR-1011