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Prototype Common Bus Spacecraft: Hover Test Implementation and ResultsIn order to develop the capability to evaluate control system technologies, NASA Ames Research Center (Ames) began a test program to build a Hover Test Vehicle (HTV) - a ground-based simulated flight vehicle. The HTV would integrate simulated propulsion, avionics, and sensors into a simulated flight structure, and fly that test vehicle in terrestrial conditions intended to simulate a flight environment, in particular for attitude control. The ultimate purpose of the effort at Ames is to determine whether the low-cost hardware and flight software techniques are viable for future low cost missions. To enable these engineering goals, the project sought to develop a team, processes and procedures capable of developing, building and operating a fully functioning vehicle including propulsion, GN&C, structure, power and diagnostic sub-systems, through the development of the simulated vehicle.
Document ID
20110014036
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Hine, Butler Preston
(NASA Ames Research Center Moffett Field, CA, United States)
Turner, Mark
(NASA Ames Research Center Moffett Field, CA, United States)
Marshall, William S.
(Research Inst. for Advanced Computer Science Moffett Field, CA, United States)
Date Acquired
August 25, 2013
Publication Date
February 26, 2009
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2009-214597/REV
ARC-E-DAA-TN556
SSPO-MLLHV-TIP-20080506
Report Number: NASA/TM-2009-214597/REV
Report Number: ARC-E-DAA-TN556
Report Number: SSPO-MLLHV-TIP-20080506
Funding Number(s)
CONTRACT_GRANT: NNA08CG83C
Distribution Limits
Public
Copyright
Public Use Permitted.
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