MIMO conditional integrator control for unmanned airlaunch

Author:

Nguyen Van Cuong1,Damm Gilney1

Affiliation:

1. IBISC - Université d'Evry Val d'Essonne; Evry France

Funder

European Union Seventh Framework Programme (FP7) Network of excellence � HYCON2 - Highly Complex and Networked Control Systems�

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Mechanical Engineering,Aerospace Engineering,Biomedical Engineering,General Chemical Engineering,Control and Systems Engineering

Reference14 articles.

1. Burlacu MM Kohlenberg J An analysis of the nanosatellites launches between 2004 and 2007 3rd International Conference on Systems and Networks Communications 2008 292 297

2. Sarigul-Klijn M Sarigul-Klijn N Selection of a carrier aircraft and a launch method for air launching space vehicles AIAA SPACE Conference and Exposition 2008 2008-7835

3. Hudson GC Quickreach responsive launch system 4th Responsive Space Conference 2006 1 5

4. Nguyen VC Damm G Azouz N Vasiljevic C Colle E Modeling and lqr robust control of an unmanned aerial vehicle for airlaunch Proceedings of 2012 International Conference on Unmanned Aircraft Systems 2012 1 6

5. Nonlinear adaptive flight control using backstepping and neural networks controller;Lee;Journal of Guidance, Control and Dynamics,2001

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1. Conditional integrator sliding mode control of an unmanned quadrotor helicopter;Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering;2021-10-06

2. Analytical Design and Stability Analysis of the Universal Integral Regulator Applied in Flight Control;International Journal of Control, Automation and Systems;2019-01-18

3. Robust attitude control for tail-sitter unmanned aerial vehicles in flight mode transitions;International Journal of Robust and Nonlinear Control;2018-12-02

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