H∞ analysis and synthesis by genetic algorithms of the attitude control system of the Brazilian Satellite launcher

European Space Agency, (Special Publication) ESA SP

Volumn , Issue 606, 2006, Pages 383-388

  Leite Filho, W C ^a   Pellanda, P C ^b   Medeiros, F E L ^c  

^a INSTITUTO DE AERONÁUTICA E ESPAÇO   (Brazil)

^b MILITARY INSTITUTE OF ENGINEERING   (Brazil)

^c Centro Tecnologico do Exercito CTEx   (Brazil)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEMS; FLIGHT DYNAMICS; GENETIC ALGORITHMS; NOTCH FILTERS; SATELLITES; THREE TERM CONTROL SYSTEMS;

BAND-REJECT (NOTCH) FILTER; BRAZILIAN SATELLITE LAUNCHER (VLS); FILTER-SWITCHING; PROPORTIONAL-INTEGRAL-DERIVATIVE (PID);

CATAPULTS (AIRCRAFT LAUNCHERS);

EID: 33646571500     PISSN: 03796566     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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2. Institute of Aeronautics and Space. A database of Brazilian launcher VLS. São José dos Campos, SP, Brazil, 1994.
3. Kienitz, K. H.; Moreira, F. J. O. Design of VLS control algorithms for movable nozzle actuators. São José dos Campos, SP, Brazil: Institute of Aeronautics and Space, 1993.
4. rd ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, Noordwijk, 1996.
5. th ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, Noordwijk, 1999.
6. Pellanda, P. C. Commande de systèmes instationnaires - séquencement de compensateurs et commande LPV. PhD Thesis, École Nationale Supérieure de l'Aéronautique et de l'Espace, ENSAE, France, 2001.
7. Pohlheim, H. Implementation of Genetic and Evolutionary Algorithms in Matlab, 1994.
8. Ramos, F. O. Perturbation due to sensor fault and its implications in design with case study (VLS). MSc dissertation. Department of Electronic Engineering, Aeronautic Technologic Institute, São José dos Campos, SP, Brazil, 2002.
9. Ramos, F. O; Leite Filho, W. C; Moreira, F. J. O. Gain computation strategy for an attitude control system. 17th International Congress of Mechanical Engineering (COBEM), 2003,
10. Voinot O., Alazard D., Apkarian P., and Mauffrey S. Launcher attitude control: discrete-time robust design and gain scheduling. Elsevier Science, 2002.