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1
Stabilization of Spacecraft Flight in Halo Orbits : An H Approach
Stabilization of Spacecraft Flight in Halo Orbits : An H Approach
J. E. Kulkarni., | Institute of Electrical and Electronics Engineers | 2006 ,
2
Time Optimal Attitude Maneuver Strategies for the Agile Spacecraft with Reaction Wheels and Thrusters
Time Optimal Attitude Maneuver Strategies for the Agile Spacecraft with Reaction Wheels and Thrusters
Byung-Hoon Lee, Bong-Un Lee, Hwa-Suk Oh, Seon-Ho, | 대한기계학회 | 2005 ,
3
Attitude Maneuver Control of Flexible Spacecraft by Observer-based Tracking Control
Attitude Maneuver Control of Flexible Spacecraft by Observer-based Tracking Control
Hyochoong Bang, Chul Han Kim, | 대한기계학회 | 2004 ,
4
Thermal Analysis of Spacecraft Propulsion System and its Validation
Thermal Analysis of Spacecraft Propulsion System and its Validation
Cho Young Han, Joon-Min Choi, | 대한기계학회 | 2004 ,
5
A Robust Control Approach for Maneuvering a Flexible Spacecraft
A Robust Control Approach for Maneuvering a Flexible Spacecraft
Yoon-Gyeoung Sung,Jea-Won Lee, | 대한기계학회 | 2001 ,
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