Mathematical techniques developed for accomplishing Earth-based guidance of unmanned lunar and interplanetary spacecraft are described; orbit determination and guidance correction aspects are developed from linear perturbation techniques; expression for effect of neglected second order terms is developed; treatment of correlated noise on orbit determination data is discussed; policies for determining when to perform impulsive guidance corrections to orbit and technique for optimal guidance of powered flight trajectories.
Guidance of unmanned lunar and interplanetary spacecraft
Progress Astronautics Aeronautics -- Celestial Mechanics Astrodynamics
1964
23 pages
Article (Journal)
English
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GUIDANCE OF UNMANNED LUNAR AND INTERPLANETARY SPACECRAFT
AIAA | 1963
|GUIDANCE OF UNMANNED LUNAR AND INTERPLANETARY SPACECRAFT
NTRS | 1963
|GUIDANCE OF UNMANNED LUNAR AND INTERPLANETARY SPACECRAFT
NTRS | 1963
|Guidance of Unmanned Lunar and Interplanetary Spacecraft
AIAA | 1964
|