Pages that link to "Item:Q364167"
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The following pages link to Attitude control for part actuator failure of agile small satellite (Q364167):
Displaying 7 items.
- Influence of flexible solar arrays on vibration isolation platform of control moment gyroscopes (Q315357) (← links)
- The output torque estimation of MCMG for agile satellites (Q358350) (← links)
- An improved constrained steering law for SGCMGs with DPC (Q358788) (← links)
- Error analysis and a new steering law design for spacecraft control system using SGCMGs (Q362974) (← links)
- Steady-state responses of a belt-drive dynamical system under dual excitations (Q739975) (← links)
- Attitude control of a rigid spacecraft with one variable-speed control moment gyro (Q740030) (← links)
- Nonlinear dynamics of axially moving viscoelastic Timoshenko beam under parametric and external excitations (Q748148) (← links)