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A plan for spacecraft automated rendezvousAn automated rendezvous approach has been developed that utilizes advances in technology to reduce real-time/near real-time flight operations support personnel to an acceptable level that is near the minimum without jeopardizing the success of the mission. The on-board flight targeting uses a rule-based system to select the pursuit vehicle phasing orbits and uses precise navigation updates from the pursuit/target spacecraft made possible by the global positioning system receivers/processors on both spacecraft to adjust the phasing orbits and achieve rendezvous. The ascent-to-orbit targeting for the pursuit vehicle has been successfully decoupled from the on-orbit orbit transfer phasing targeting. Typical launch window data have been developed for the heavy lift launch vehicle and cargo transfer vehicle for a Space Station Freedom rendezvous mission.
Document ID
19930006203
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Deaton, A. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lomas, J. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Mullins, L. D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Subject Category
Astrodynamics
Report/Patent Number
NASA-TM-108385
NAS 1.15:108385
Report Number: NASA-TM-108385
Report Number: NAS 1.15:108385
Accession Number
93N15392
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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