Aircraft simulation and control

• المؤلف الرئيسي: Zhao, Liang.
• مؤلفون آخرون: Wang Jianliang
• التنسيق: Theses and Dissertations
• اللغة: English
• منشور في: 2009
• الموضوعات: DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/18758

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...