Pages that link to "Item:Q357805"
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The following pages link to Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel (Q357805):
Displaying 10 items.
- Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators (Q295600) (← links)
- Reduction of large-scale dynamical systems by the Krylov subspaces method: analysis of approaches (Q499130) (← links)
- Momentum unloading excessive reaction-wheel system of a spacecraft (Q734021) (← links)
- Synthesis of spacecraft covariance controls (Q895307) (← links)
- Methods for suppressing nonlinear oscillations in astatic auto-piloted aircraft control systems (Q1745835) (← links)
- Terminal synthesis of orbital orientation for a spacecraft (Q1745868) (← links)
- Algorithms for the synthesis of observers for nonlinear dynamic systems (Q2017643) (← links)
- Schemes of momentum/reaction wheels unloading by mechanical restructuring and gearbox for spacecraft (Q2076279) (← links)
- Synthesis of decoupling laws for attitude stabilization of a spacecraft (Q2263388) (← links)
- Annihilation of Transverse Velocity Bias During Spinning-Up Maneuvers (Q4370715) (← links)
