Pages that link to "Item:Q3644975"
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The following pages link to Spacecraft attitude control by combination of various torquers (Q3644975):
Displaying 5 items.
- The output torque estimation of MCMG for agile satellites (Q358350) (← links)
- The coupling characteristic investigation of double-gimbal magnetically suspended control moment gyro used on agile maneuver spacecraft (Q1665210) (← links)
- Decentralised finite-time attitude synchronisation and tracking control for rigid spacecraft (Q2792186) (← links)
- Attitude Control of a Spacecraft with Two Reaction Wheels (Q5699632) (← links)
- Design and validation of an MPC controller for CMG-based testbed (Q6159474) (← links)