Direct parametric attitude tracking control for generic hypersonic vehicle
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Publication:5027549
DOI10.1080/00207721.2018.1457732zbMath1482.93204OpenAlexW2800101799WikidataQ129979544 ScholiaQ129979544MaRDI QIDQ5027549
Publication date: 4 February 2022
Published in: International Journal of Systems Science (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/00207721.2018.1457732
Related Items (3)
Output strictly passive \(H_\infty\) control of discrete-time linear switched singular systems via proportional plus derivative state feedback ⋮ Novel smooth sliding mode attitude control design for constrained re-entry vehicle based on disturbance observer ⋮ A novel non-uniform optimal control approach for hypersonic cruise vehicle with waypoint and no-fly zone constraints
Cites Work
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- Complete parametric approach for eigenstructure assignment in a class of second-order linear systems
- Adaptive sliding mode tracking control for a flexible air-breathing hypersonic vehicle
- Linear parameter varying switching attitude control for a near space hypersonic vehicle with parametric uncertainties
- Generalized Sylvester Equations
- Solution to the second-order Sylvester matrix equation MVF/sup 2/+DVF+KV=BW
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