Pages that link to "Item:Q4006392"
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The following pages link to Aircraft flight controls design using output feedback (Q4006392):
Displaying 14 items.
- Geometric pseudospectral method on \(SE(3)\) for rigid-body dynamics with application to aircraft (Q474413) (← links)
- Resolving actuator redundancy--optimal control vs. control allocation (Q705452) (← links)
- Nonlinear simulation of controller for longitudinal control augmentation system of F-16 using numerical approach (Q707335) (← links)
- Real-time fixed-order lateral \(H_2\) controller for micro air vehicle (Q763137) (← links)
- Guaranteed cost control of a Markov jump linear uncertain system using a time-multiplied cost function (Q1411394) (← links)
- Suboptimal regulators for discrete-time jump linear systems with time-multiplied performance index (Q1810923) (← links)
- Optimal input design for aircraft stability and control flight testing (Q2055339) (← links)
- Flight systems and control. A practical approach (Q2330303) (← links)
- Finite-time stabilization via dynamic output feedback (Q2491923) (← links)
- Finite modeling of parabolic equations using Galerkin methods and inverse matrix approximations (Q2563555) (← links)
- (Q3340573) (← links)
- High‐gain output feedback for a miniature UAV (Q5166492) (← links)
- Compensating periodic descriptor systems (Q5941039) (← links)
- Design of reduced-order observer based steady state optimal linear-quadratic feedback controllers (Q6579242) (← links)
