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Study on Orbital Characteristics and Control of Hovering Spacecraft
Author: ZhuYaWen
Tutor: ZuoYe
School: National University of Defense Science and Technology
Course: Aeronautical and Astronautical Science and Technology
Keywords: Hover track Hover configuration remains Nominal control acceleration Deviation control acceleration Energy consumption T-H equation LQR control
CLC: V448
Type: Master's thesis
Year: 2010
Downloads: 103
Quote: 0
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Abstract
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CLC: > Aviation, aerospace > Aerospace ( Astronauts ) > Space instrument,spacecraft devices,spacecraft guidance and control > Guidance and Control
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