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Rendezvous Integration Complexities of NASA Human Flight VehiclesPropellant-optimal trajectories, relative sensors and navigation, and docking/capture mechanisms are rendezvous disciplines that receive much attention in the technical literature. However, other areas must be considered. These include absolute navigation, maneuver targeting, attitude control, power generation, software development and verification, redundancy management, thermal control, avionics integration, robotics, communications, lighting, human factors, crew timeline, procedure development, orbital debris risk mitigation, structures, plume impingement, logistics, and in some cases extravehicular activity. While current and future spaceflight programs will introduce new technologies and operations concepts, the complexity of integrating multiple systems on multiple spacecraft will remain. The systems integration task may become more difficult as increasingly complex software is used to meet current and future automation, autonomy, and robotic operation requirements.
Document ID
20090007819
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Brazzel, Jack P.
(NASA Johnson Space Center Houston, TX, United States)
Goodman, John L.
(United Space Alliance Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
January 30, 2009
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-17709
AAS 09-065
Report Number: JSC-17709
Report Number: AAS 09-065
Meeting Information
Meeting: 2009 AAS GN&C Conference
Location: Virginia
Country: United States
Start Date: January 30, 2009
End Date: February 4, 2009
Sponsors: American Astronautical Society
Funding Number(s)
CONTRACT_GRANT: NNJ06VA01C
Distribution Limits
Public
Copyright
Public Use Permitted.
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