@inproceedings{38d848b244cb4ffcb06a8df782158c96,
title = "An analytical design method for the missile two-loop acceleration autopilot",
abstract = "According to the missile longitudinal dynamics expressed as the state space matrix form and the defined dynamics coefficient notations, the missile body transfer functions are deduced in detail. Using the thought of pole allocation, a detailed analytical methodology for designing the two-loop acceleration autopilot has been proposed. To get the exact gain crossover frequency of the autopilot, an unconstraint optimization problem is outlined. The design and simulation results show that the two-loop acceleration autopilot can stabilize the missiles with different static margins very well.",
keywords = "analytical methodology, missile, static margin, two-loop autopilot",
author = "Hui Wang and Defu Lin and Jiaxin Wang and Tao Song",
year = "2012",
doi = "10.1007/978-3-642-34381-0_18",
language = "English",
isbn = "9783642343803",
series = "Communications in Computer and Information Science",
number = "PART 1",
pages = "157--165",
booktitle = "System Simulation and Scientific Computing - International Conference, ICSC 2012, Proceedings",
edition = "PART 1",
note = "Asia Simulation Conference and the International Conference on System Simulation and Scientific Computing 2012, AsiaSim and ICSC 2012 ; Conference date: 27-10-2012 Through 30-10-2012",
}