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Spacecraft attitude control during thrusting maneuvers, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance And Control)

NASA/SP-8059, Spacecraft attitude control during thrusting maneuvers, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance And Control), NASA (Washington, DC, United States), February,1971, pp. 51, Format(s): PDF 2970k

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Systems design criteria for spacecraft attitude control during thrusting maneuvers
Keywords:navigation, satellite attitude control, spacecraft maneuvers, systems engineering, thrust vector control, computerized simulation, performance tests, spin stabilization, stationkeeping
CASI Document ID Number:71N26198
Subjects:Astronautics: Spacecraft Design, Testing And Performance: Spacecraft Attitude Control And Stabilization
ID Code:97
Deposited On:15 May 2002