DocumentCode :
486744
Title :
Trajectory Shaping Rendezvous Guidance
Author :
Klumpp, Allan R.
Author_Institution :
Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, California 91109
fYear :
1986
fDate :
18-20 June 1986
Firstpage :
1545
Lastpage :
1550
Abstract :
The Space Station will bring a great increase in rendezvous traffic. Formerly, rendezvous has been expensive in terms of time and crew involvement. Multiple trajectory adjustments on separate orbits have been requird to meet safety, lighting, and geometry requirements. This paper describes a new guidance technique in which the approach trajectory is shaped by a sequence of velocity increments in order to satisfy multiple constraints within a single orbit. The approach phase is planned before the mission, leaving a group of free parameters that are optimized by onboard guidance. Fuel penalties are typically a few percent, compared to unshaped Hohmann transfers, and total fuel costs can be less than those of more time-consuming ways of meeting the same requirements.
Keywords :
Costs; Fuels; Geometry; Navigation; Orbits; Safety; Space stations; Space technology; Space vehicles; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1986
Conference_Location :
Seattle, WA, USA
Type :
conf
Filename :
4789171
Link To Document :
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