OPTIMAL MULTIPLE-IMPULSE TIME-FIXED RENDEZVOUS BETWEEN CIRCULAR ORBITS.

被引：0

作者：

Prussing, John E. ^{[1
]}

Chiu, Jeng-Hua ^{[1
]}

机构：

[1] Univ of Illinois at, Urbana-Champaigne, Dep of, Aeronautical & Astronautical, Univ of Illinois at Urbana-Champaigne, Dep of Aeronautical & Astronautical Engineering, Urbana,

来源：

| 1600年 / 09期

关键词：

Theoretical; (THR);

D O I：

暂无

中图分类号：

学科分类号：

摘要：

(Edited Abstract)

引用

共 50 条

[41] OPTIMAL COOPERATIVE POWER-LIMITED RENDEZVOUS BETWEEN NEIGHBORING CIRCULAR ORBITS - REPLY
COVERSTONECARROLL, V
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1995, 18 (05) : 1224 - 1224
[42] A METHOD FOR DETERMINING OPTIMAL FIXED-TIME N-IMPULSE TRAJECTORIES BETWEEN ARBITRARILY INCLINED ORBITS
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ASTRONAUTICA ACTA, 1969, 14 (04): : 358 - &
[43] OPTIMAL IMPULSIVE TIME-FIXED DIRECT-ASCENT INTERCEPTION
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[44] Extremal impulse transfers between close coplanar circular orbits with time restriction
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[45] Constant-thrust glideslope guidance algorithm for time-fixed rendezvous in real halo orbit
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[46] Six-impulse maneuvers for rendezvous of spacecraft in near-circular noncoplanar orbits
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[47] Six-impulse maneuvers for rendezvous of spacecraft in near-circular noncoplanar orbits
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[48] ORBIT TRANSFER AND RENDEZVOUS MANEUVERS BETWEEN INCLINED CIRCULAR ORBITS
BAKER, JM
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[49] EXTREMAL IMPULSE TRANSFERS BETWEEN CLOSE COPLANAR CIRCULAR ORBITS WITH TIME RESTRICTION CONDITION
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[50] OPTIMAL RENDEZVOUS MANOEUVRE OF SPACE VEHICLES ON CIRCULAR ORBITS WITH MINIMAL FUEL CONSUMPTION
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ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1968, 16 (04): : 115 - +

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