Non Linear Dynamic Inversion Technique
Over the last two decades or so, control researchers have begun to apply alternative methodologies to flight control design. One alternative is variously called non-linear dynamic inversion or feedback linearization. The purpose of dynamic inversion is to develop a feedback control law that lineariz...
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| Formato: | capítulo de livro |
| Fecha de publicación: | 2007 |
| País: | España |
| Recursos: | Universidad Nacional de Educación a Distancia |
| Repositorio: | e-spacio. Repositorio Institucional de la UNED |
| Idioma: | inglés |
| OAI Identifier: | oai:e-spacio.uned.es:20.500.14468/15622 |
| Acesso em linha: | https://hdl.handle.net/20.500.14468/15622 |
| Access Level: | acceso abierto |
| Palavra-chave: | ROBUST CONTROL TECHNIQUES Non Linear Dynamic Inversion Technique |
| Resumo: | Over the last two decades or so, control researchers have begun to apply alternative methodologies to flight control design. One alternative is variously called non-linear dynamic inversion or feedback linearization. The purpose of dynamic inversion is to develop a feedback control law that linearizes the plant response to commands. Simple controllers can then be designed. With dynamic inversion, a non-linear control law is designed which globally reduces the dynamics of selected controlled variables to integrators. A closed loop system is then designed to make the controlled variables exhibit specified command responses while satisfying the usual disturbances response and robustness requirements for the overall system and the various physical limitations of the aircraft’s control effectors. |
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