Design Method Research on Autopilot of Rolling Missile

DOI

10.2991/acta-14.2014.25How to use a DOI?

Keywords

Autopilot design; rolling missile; coherence research; actuator delay

Abstract

The theory on autopilot design of non-rolling missile has been well developed, but the perfect theory on autopilot design of rolling missile has not come into being. Aiming at this problem, the coherence research on autopilot is carried out based on the analysis of scope and frequency area. And the primary coherence condition is given. With the research work, it is expected that the answer can be gotten about with which condition controller design of rolling missile can be translated into controller design of non-rolling missile. Finally, the actuator delay problem of rolling missile is researched, too.

Copyright

© 2014, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Yuan Bo
AU  - Yang Jun
PY  - 2014/06
DA  - 2014/06
TI  - Design Method Research on Autopilot of Rolling Missile
BT  - 2014 International Conference on Automatic Control Theory and Application
PB  - Atlantis Press
SP  - 100
EP  - 103
SN  - 2352-5398
UR  - https://doi.org/10.2991/acta-14.2014.25
DO  - 10.2991/acta-14.2014.25
ID  - Bo2014/06
ER  -