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Numerical SDRE Approach for Missile Integrated Guidance - Control
AIAA Guidance, Navigation and Control Conference and Exhibit, 2007‡Numerical s tate -dependent Riccati equation based integrated guidance -control formulation is developed for an internally actuated missile. The dynamic system under consideration is of tenth order , making it tedious to algebraically manipulate the equations of motion into the state -dependent coeffic ient form central to the design methodology .
Sesha Vaddi +2 more
openaire +1 more source
Magnetic levitation system controlled by SDRE control
Anais do X Congresso Nacional de Engenharia Mecânica, 2018Rodrigo Tumolin Rocha +3 more
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Spacecraft formation flying control around L2 sun-earth libration point using on–off SDRE approach
Advances in Space Research, 2021Hossein Rouzegar +2 more
exaly
Tracking Control of Control Moment Gyroscope Using SDRE Method
The Proceedings of Conference of Tokai Branch, 2018Reina NAKAGAMI, Isao TAKAMI, Gan Chen
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SDRE based optimal finite-time tracking control of a multi-motor driving system
International Journal of Control, 2021Qiang Chen, Minlin Wang
exaly
Application of SDRE control to Hybrid Remotely Operated Vehicle
Proceedings of the 26th International Congress of Mechanical Engineering, 2021Allan Oliveira +3 more
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Acta Crystallographica Section F: Structural Biology Communications, 2010
Hua Xiang, Shentao Li
exaly
Hua Xiang, Shentao Li
exaly
Robust SDRE filter design for nonlinear uncertain systems with an performance criterion
ISA Transactions, 2012Hossein Beikzadeh, Hamid D Taghirad
exaly