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Conference papers
Robust stabilization of an airlaunch system after launching phase
Abstract : A Multiple Input Multiple Output (MIMO) controller based on the dynamic feedback linearization technique is designed for the robust global stabilization of a new satellite launching strategy called (unmanned) airlaunch. This strategy consists in using a two-stages launching system. The first stage is composed of an airplane (manned or unmanned) that carries a rocket launcher which constitute the subsequent stages. The control objective is to stabilize the aircraft in the launch phase. It is developed and is applied to the full multi-input multi-output model of the aircraft. The considered model is highly nonlinear, mostly as a consequence of possible large angle of attack, sideslip and roll angle. Finally, the present work illustrates through simulations the good performance of the proposed control algorithm.
https://hal.archives-ouvertes.fr/hal-00786859
Contributor : Frédéric Davesne Connect in order to contact the contributor
Submitted on : Tuesday, March 30, 2021 - 10:32:08 PM
Last modification on : Saturday, May 1, 2021 - 3:39:37 AM
Contributor : Frédéric Davesne Connect in order to contact the contributor
Submitted on : Tuesday, March 30, 2021 - 10:32:08 PM
Last modification on : Saturday, May 1, 2021 - 3:39:37 AM
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CDC2012final__VCN_RM_GD.pdf
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