Pages that link to "Item:Q5048712"
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The following pages link to Pitch and yaw motion control of 2 DoF helicopter subjected to faults using sliding-mode control (Q5048712):
Displaying 6 items.
- Output sliding mode-based stabilization of underactuated 3-DOF helicopter prototype and its experimental verification (Q1660413) (← links)
- Composite control of a hovering helicopter based on optimized sliding mode control (Q2055361) (← links)
- Adaptive quantized fault-tolerant control of a 2-DOF helicopter system with actuator fault and unknown dead zone (Q2682332) (← links)
- A novel fault classification‐based fault‐tolerant control for <scp>two degree of freedom</scp> helicopter systems (Q5000728) (← links)
- Extended state observer‐based sliding mode fault‐tolerant control for unmanned autonomous helicopter with wind gusts (Q5221157) (← links)
- An optimal hybrid quadcopter control technique with MPC-based backstepping (Q6577189) (← links)
