Flight Vehicle includes aircraft, spacecraft, rocket and missile. Attitude tracking and stabilization are key technologies of modern flight vehicle systems which have been served as an interesting benchmark in the past decades. In the attitude equations, two types of uncertainties are paid attention widely, one is the external disturbance which arises from the unexpected environmental torques, and another is the model uncertainty existing in the inertia matrix of the spacecraft. The presence of the external disturbance and the inertia uncertainty makes the attitude control problem more complicated. From a practical point of view, the design of efficient and low-cost attitude controllers is an important issue for aerospace industry.


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    Title :

    Overview of Flight Vehicle Control


    Additional title:

    Lect.Notes Control


    Contributors:
    Xia, Yuanqing (author) / Fu, Mengyin (author)


    Publication date :

    2013-01-01


    Size :

    6 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Overview of Flight Vehicle Control

    Xia, Yuanqing / Fu, Mengyin | Tema Archive | 2013





    Flight Control Technology: An Overview

    Siouris, G. M. / International Federation of Automatic Control | British Library Conference Proceedings | 1999