%0 Journal Article
%T Application of PID controller to 2D differential geometric guidance problem<br>
%A Chaoyong LI
%A Wuxing JING
%A <br>
%J 控制理论与应用
%D 2007
%I 
%X This paper presents the application of the proportional-integral-derivative (PID) controller to the flight control system (FCS) for two-dimensional (2D) differential geometric (DG) guidance and control problem. In particular, the performance of the designed FCS is investigated. To this end, the commanded angle-of-attack is firstly developed in the time domain using the classical DG formulations. Then, the classical PID controller is introduced to develop a FCS so as to form the 2D DG guidance and control system, and the PID controller parameters are determined by the Ziegler-Nichols method as well as the Routh-Hurwitz stability algorithm to guarantee the convergence of the system error. The results demonstrate that the designed controller yields a fast responding system, and the resulting DG guidance and control system is viable and effective in a realistic missile defense engagement.
%K Differential geometry
%K Flight control system
%K Missile guidance
%K PID controller<br>
%U http://www.alljournals.cn/get_abstract_url.aspx?pcid=5B3AB970F71A803DEACDC0559115BFCF0A068CD97DD29835&cid=8240383F08CE46C8B05036380D75B607&jid=970898A57DFC021F93AB51667BAED7F7&aid=AC1201C33B3F6D5653A6DC7381088C45&yid=A732AF04DDA03BB3&vid=94C357A881DFC066&iid=38B194292C032A66&sid=B8F8200D88DDC7D6&eid=211C7E02AC474301&journal_id=1000-8152&journal_name=控制理论与应用&referenced_num=0&reference_num=0