A Novel BTT and STT Switch Control for Surface-to-Air Missiles

DOI

10.2991/mbdasm-19.2019.32How to use a DOI?

Keywords

Coordinated BTT; STT; switch control

Abstract

To solve the problems that bank-to-turn (BTT) control is highly coupled and do not have a fast response time as well as that skid-to-turn (STT) control lacks of flying stability, this paper divides flight time of surface-to-air missile (SAM) into two stages by fully taking the advantages of both BTT and STT control. In this paper, Coordinated BTT controller and STT controller are designed to control angle of attack, sideslip angle and rolling angle. Based on the distance between target and missile, the switch control logics changes from coordinated BTT control to STT control to ensure the stability, response time and mobility of flight. The simulation in the paper proves the validity and stability of this method.

Copyright

© 2019, 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  - Zhaoliang Zheng
PY  - 2019/10
DA  - 2019/10
TI  - A Novel BTT and STT Switch Control for Surface-to-Air Missiles
BT  - Proceedings of the 2019 International Conference on Mathematics, Big Data Analysis and Simulation and Modelling (MBDASM 2019)
PB  - Atlantis Press
SP  - 139
EP  - 142
SN  - 2352-538X
UR  - https://doi.org/10.2991/mbdasm-19.2019.32
DO  - 10.2991/mbdasm-19.2019.32
ID  - Zheng2019/10
ER  -