Contacto
Como comprar
Entrega
Guia de compras
Nonlinear Autopilot Design for Aerospace Vehicles
Inglês
199 b
Até 30 dias para devoluções
Os clientes também compraram
/
Adobe ePub DRM
1.10
€
/
Capa mole
34.87
€
Traditionally, missile autopilots have been designed using linear control approaches with gain scheduling. Moreover, three single axis autopilots are usually designed without considering the interaction among the motion axes. Such designs cannot handle the coupling among pitch-yaw-roll channels, especially under high angles of attack occurring in high maneuver zones. In most research studies, realistic factors like fin saturation, limitation of gimbal freedom etc are not considered. Our research work contributed a nonlinear multivariable approach to the design of an autopilot for a realistic missile that overcomes these difficulties. At first, exact input-output (IO) feedback linearization and decoupling is carried out for the dynamic IO characteristics of the inner rate loop of the pitch and yaw channels. This enables the design of scalar linear controllers for the inner rate loops. However performance deteriorates when the plant model is perturbed, due to aerodynamic uncertainties, from the nominal model. The robust IO linearization techniques are developed using H_inf and sliding mode techniques.
Sobre o livro
Inglês
Ofereça este livro hoje
É fácil
1 Adicione ao carrinho e escolha Entregar como presente ao finalizar a compra 2 Receberá um vale 3 O livro chegará ao endereço do destinatárioTambém pode estar interessado em
/
Adobe ePub DRM
5.45
€
/
Capa mole
11.21
€
/
Livro de capa dura
26.88
€
/
Capa mole
10.30
€
Olá! Sou o Libroamiko, o seu conselheiro de livros.
Como posso ajudar?