@inproceedings{e9cce82249684a6aaa4aed678cd6b573,
title = "Air-launched rocket attitude control of separation stage based on RCS",
abstract = "In this paper, attitude control problem of carbin airlaunching duing separation stages between plane and vehicle by reaction control system (ReS) was studied. First analyzed movement under different separation conditions between launch rocket and plane, then determined launch vehicle flight status when ReS fired and designed rocket pitching program. On this basis, given the standard trajectory programs and ReS configuration. Using pulse width and pulse frequency modulation method, ReS thruster switch controller is designed. The simulation results show the correctness of ReS thruster configuration.",
keywords = "Air-launched, Component, Control system, Reaction control system",
author = "Zhi Xu and Shuo Tang",
year = "2010",
doi = "10.1109/ICACTE.2010.5579561",
language = "英语",
isbn = "9781424465408",
series = "ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings",
pages = "V3619--V3622",
booktitle = "ICACTE 2010 - 2010 3rd International Conference on Advanced Computer Theory and Engineering, Proceedings",
note = "2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010 ; Conference date: 20-08-2010 Through 22-08-2010",
}