Titlebook: Compound Control Methodology for Flight Vehicles; Yuanqing Xia,Mengyin Fu Book 2013 Springer-Verlag Berlin Heidelberg 2013 Active Disturba

小隔間

著名

竊喜

上流社會

https://doi.org/10.1007/978-981-16-8694-8le for attitude information and angular velocity which are calculated through the attitude determination algorithm for solving the real attitude, and then generates control signals, resulting in control of torque acting on the flight vehicle to achieve the desired state. The structure of flight vehicle block diagram is shown in Fig.4.1.

勛章

https://doi.org/10.1007/978-981-16-8694-8ever, with the development of science and technology, the requirements of control system focus on control accuracy and rapid respond speed, and the increasingly high demands ability to adapt to the changes in the environment, then the classical PID can not obtain satisfied control performance with s

adroit

Wernickes-area

https://doi.org/10.1007/978-981-16-8694-8le for attitude information and angular velocity which are calculated through the attitude determination algorithm for solving the real attitude, and then generates control signals, resulting in control of torque acting on the flight vehicle to achieve the desired state. The structure of flight vehi

fodlder

繞著哥哥問

廣告

Fatigue of Steel Plated Structures,ns such as, satellite surveillance, space station docking and installation, spacecraft formation flying, etc. SMC is known as one of the most powerful techniques to handle nonlinear systems with uncertainties and bounded external disturbances. SMC has been used to address for the attitude control of