Pages that link to "Item:Q5027549"
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The following pages link to Direct parametric attitude tracking control for generic hypersonic vehicle (Q5027549):
Displaying 4 items.
- Output strictly passive \(H_\infty\) control of discrete-time linear switched singular systems via proportional plus derivative state feedback (Q2193637) (← links)
- Trajectory control of a high altitude hypervelocity flying vehicle in the midcourse active phase of the flight (Q2263838) (← links)
- Novel smooth sliding mode attitude control design for constrained re-entry vehicle based on disturbance observer (Q5025816) (← links)
- A novel non-uniform optimal control approach for hypersonic cruise vehicle with waypoint and no-fly zone constraints (Q5029122) (← links)