@inproceedings{29c1756a1d894d0d9dd196390b6b71c5,
title = "Design and comparison of classical topologies for static unstable missile autopilots",
abstract = "The characteristics and benefit of applying relaxed static stability technology on missile flight performance were presented. The transform technologies both of engineering index into the desired system poles and state feedback into output feedback were analyzed. Based on optimization and output feedback, a general design methodology for multiple topologies of autopilots was proposed. The analysis is accomplished by establishing a standard algorithm for different autopilot topologies. Anyone of the two- and three-loop autopilots can stabilize a static unstable missile. However, the finite resource of actuator is the crucial factor for autopilot control effect.",
keywords = "Actuator resource, Output feedback, Relaxed static stability, Static unstable missile",
author = "Fan, {Jun Fang} and Xia, {Qun Li} and Qi, {Zai Kang}",
year = "2008",
doi = "10.1109/CCDC.2008.4598013",
language = "English",
isbn = "9781424417346",
series = "Chinese Control and Decision Conference, 2008, CCDC 2008",
pages = "3659--3664",
booktitle = "Chinese Control and Decision Conference, 2008, CCDC 2008",
note = "Chinese Control and Decision Conference 2008, CCDC 2008 ; Conference date: 02-07-2008 Through 04-07-2008",
}