Title :
A Nonovershooting Pitch-Angle Regulator for Aircraft with Conventional Aerodynamic Configuration
Author :
Liang, Shuguo ; Chen, Xiaoping ; Zhu, Bo
Author_Institution :
Inst. of Astronaut. & Aeronaut., Univ. of Electron. Sci. & Technol. of China, Chengdu, China
Abstract :
The problem of designing a nonovershooting controller for general high-order linear time-invariant plants is still open. In this paper, we propose a new technique to design nonovershooting pitch-angle regulator for conventional aircraft based on the forth-order model of longitudinal motion. The regulator is composed of the error-feedback and the feed forward control terms. Two forms of the regulator are presented which apply to the state-feedback and the output feedback cases, respectively. Simulation examples are given to show the effectiveness of the regulator.
Keywords :
aerodynamics; aircraft control; feedforward; motion control; state feedback; aircraft; conventional aerodynamic configuration; error feedback; feedforward control terms; forth order longitudinal motion model; high order linear time invariant plants; nonovershooting controller; nonovershooting pitch-angle regulator; state feedback; Aerodynamics; Aircraft; Atmospheric modeling; Mathematical model; Observers; Regulators; State feedback; Attitude control; nonovershooting regulator; output feedback; state feedback;
Conference_Titel :
Intelligent Computation Technology and Automation (ICICTA), 2012 Fifth International Conference on
Conference_Location :
Zhangjiajie, Hunan
Print_ISBN :
978-1-4673-0470-2
DOI :
10.1109/ICICTA.2012.134
