Modeling and Control - Flexible Structure Spacecraft

Installation dynamics, optimal thruster propulsion, and specific impulse thrust for reignitable fuel motors to regulate pointing error is obtained for geosynchronous (e.g., the Indian National Satellite, INSAT

• Type: Journal
• Year: 2002
• Where: INFORMATICALT
• Authors: Harcharan S. Kang
• Keywords: Indian National Satellite, INFORMATICALT 2002, Optimal Thruster Propulsion, Satellite