Pages that link to "Item:Q5188395"
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The following pages link to Control of Three-axis Stabilized Flexible Spacecraft Using Variable Structure Strategies Subject to Input Nonlinearities (Q5188395):
Displaying 15 items.
- Fault-tolerant sampled-data control of flexible spacecraft with probabilistic time delays (Q494756) (← links)
- Robust control of non-linear flexible spacecraft (Q711366) (← links)
- Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits (Q840286) (← links)
- Sliding mode maneuvering control and active vibration damping of three-axis stabilized flexible spacecraft with actuator dynamics (Q840431) (← links)
- Design of discrete control system of flexible spacecraft maintaining robust stability of elastic oscillations (Q1040489) (← links)
- Output regulation of a flexible spacecraft with exponentially stable/unstable internal dynamics (Q1267267) (← links)
- Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft (Q1634453) (← links)
- Disturbance observer based \(H_\infty\) control for flexible spacecraft with time-varying input delay (Q1648699) (← links)
- Robust fault-tolerant control for flexible spacecraft against partial actuator failures (Q2348202) (← links)
- Robust and adaptive variable structure output feedback control of uncertain systems with input nonlinearity (Q2440633) (← links)
- Adaptive variable structure maneuvering control and vibration reduction of three-axis stabilized flexible spacecraft (Q2512081) (← links)
- (Q3540644) (← links)
- Variable structure controller design for spacecraft nutation damping (Q3752262) (← links)
- Guaranteed Performance Control of Nonlinear Systems with Application to Flexible Space Structure (Q4842224) (← links)
- Research on Variable Structure and Adaptive Control for Strap-on Rocket (Q5368160) (← links)
