基于倾转翼飞机垂直起降阶段PID姿态控制器设计
Design of PID Attitude Controller for Tilt Rotor in VTOL Mode
摘要:
倾转翼飞机克服了倾转旋翼飞机垂直起降状态因固定机翼阻挡旋翼下洗气流而造成的效率降低的问题，但仍存在姿态控制难问题。然后针对倾转翼飞机垂直起降阶段的姿态控制提出相应的控制方案，并对俯仰和横滚姿态控制建立了数学模型和采用PID控制方法设计了相应的姿态控制器，最后使用Matlab软件平台的Simulink模块对该PID控制方法的可行性和有效性进行仿真验证。结果表明，俯仰和横滚姿态控制器均能满足要求。
Abstract:
The tilt wing aircraft overcomes the problem that the efficiency of the wing rotor IS reduced due to the lower air flow caused by the fixed wing blocking rotor, but there are still problems of attitude control. Then the corresponding control scheme is put forward for the attitude of the tilt wing aircraft in VTOL mode, and focuses on the pitch and roll attitude control mathematical model are established and the attitude controller is designed by using PID control method. Finally, the simulink module of Matlab software platform is used to simulate the feasibility and validity of the PID control method.
参考文献
|
[1]
|
徐敏. 倾转旋翼机的发展与关键技术综述[J]. 直升机技术, 2003(2): 40-46.
|
|
[2]
|
凌和生. 新型垂直起降飞机V22鱼鹰偏转旋翼机[J]. 江苏航空, 2017(1): 18-20.
|
|
[3]
|
Martin, D. and Maisel, D.C. (2000) The Histroy of the XV-15 Tilt Rotor Research Aircraft: From Concept to Flight. NASA Publication, Washington DC, 45-47.
|
|
[4]
|
宋彦国, 王焕瑾, 沙虹伟, 等. 倾转旋翼飞行器飞行力学模型研究[J]. 空气动力学学报, 2008(2): 192-196.
|
|
[5]
|
杨军, 吴希明, 凡永华, 等. 倾转旋翼飞行器飞行控制[M]. 北京: 航空工业出版社, 2006: 45-56.
|
|
[6]
|
王岩. 倾转四旋翼无人机垂直起降阶段控制系统研究[D]: [硕士学位论文]. 哈尔滨: 哈尔滨工业大学, 2013
|
|
[7]
|
徐昊. 倾转旋翼机姿态控制问题研究[D]: [硕士学位论文]. 哈尔滨: 哈尔滨工业大学, 2011.
|
|
[8]
|
Reber, R. (1995) Intermodal Air Facilities for the 21st Century. TransTech Conference, Seattle, 30 July-2 August 1995, 54-62.
https://doi.org/10.1109/prttc.1995.518063
|
|
[9]
|
Farid, K., Isabelle, F. and Rogelio, L. (2005) Modeling and Control of a Small Autonomous Aircraft Having Two Tilting Rotors. 44th IEEE Conference on Decision and Control, and the European Control Conference, Deville, 8144-8149.
|
|
[10]
|
张德丰. MATLAB自动控制系统设计[M]. 北京: 机械工业出版社, 2010: 285-294.
|