Design of an attitude control system by multi objective optimization considering practical operation of spacecraft equipped with control moment gyros

Physics & Astronomy

• attitude control 100%
• gyroscopes 75%
• spacecraft 62%
• moments 49%
• maneuverability 48%
• optimization 45%
• gimbals 44%
• settling 34%
• requirements 26%
• spacecraft control 17%
• actuators 16%
• life (durability) 13%
• torque 9%
• numerical analysis 9%
• evaluation 6%

Engineering & Materials Science

• Attitude control 75%
• Multiobjective optimization 64%
• Spacecraft 61%
• Control systems 42%
• Maneuverability 40%
• Actuators 17%
• Numerical analysis 9%
• Torque 8%

Earth & Environmental Sciences

• control system 67%
• spacecraft 63%
• evaluation criterion 16%
• design method 15%
• torque 15%
• parameter 14%
• analysis 3%