Aircraft simulation and control

• 主要作者: Zhao, Liang.
• 其他作者: Wang Jianliang
• 格式: Theses and Dissertations
• 語言: English
• 出版: 2009
• 主題: DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
• 在線閱讀: http://hdl.handle.net/10356/18758
• 機構: Nanyang Technological University

This dissertation aims at F-16 fighter to design controller and to make simulation for analyzing its performance under specific condition. Nonlinear plants model of F-16 derived from the kinematics and dynamics of aircraft is first given, which provides a necessary precondition for analyzing and res...