[1] 罗倩兰.基于RBF-ARX模型的预测控制在四旋翼飞行器控制系统中的应用[D］.长沙: 中南大学,2012.

[2] KUTAY A T,CALISE A J,IDAN M,et al.Experimental results on adaptive output feedback control using a labora-tory model helicopter[J］.IEEE Transactions on Control Systems Technology,2005,13(2):196-202.

[3] LU X H,LI J B,LIU W J.A study of complementary filter algorithm for four-rotor helicopters attitude control system[J］.Sensors & Transducers,2014,174(7): 298-306.

[4] 赵元伟,卢京朝.四旋翼飞行器的建模及基于反步法的控制[J］.科学技术与工程,2013,13(34):10425-10430.

[5] ZHENG B,ZHONG Y S.Robust attitude regulation of a 3-DOF helicopter benchmark:theory and experiments[J］.IEEE Transactions on Industrial Electronics,2011,58(2): 660-670.

[6] KUMAR M V,SAMPATH P,SURESH S,et al.Design of a stability augmentation system for a helicopter using LQR control and ADS-33 handling qualities specifications[J］.Aircraft Engineering and Aerospace Technology,2008,80(2):111-123.

[7] 席裕庚,李德伟,林姝.模型预测控制——现状与挑战[J］.自动化学报,2013,39(3):222-236.

[8] 盖俊峰,赵国荣,周大旺.刚体飞行器姿态机动的模型预测控制方法[J］.弹箭与制导学报,2015,35(2):5-9.

[9] 高海燕,蔡远利.高超声速飞行器的滑模预测控制方法[J］.西安交通大学学报,2014,48(1):67-72.

[10] 孙光,朱如意,王征.基于干扰观测器的飞行器再入姿态广义预测控制[J］.航天控制,2016,34(4):10-15.

[11] 胡超芳,任艳丽,解倩倩.基于RMPC的高超声速飞行器输入饱和控制[J］.航天控制,2016,34(2):20-26.

[12] 张聚.显式模型预测控制理论与应用[M］.北京: 电子工业出版社,2015.

[13] 魏吉敏.四旋翼飞行器的建模及预测控制研究[D］.长沙: 中南大学,2013.

[14] BEMPORAD A,MORARI M,DUA V,et al.The explicit linear quadratic regulator for constrained systems [J］.Automatica,2002,38(1):3-20.

[15] PANOS C,KOURAMAS K I,GEORGIADIS M C,et al.Modelling and explicit model predictive control for PEM fuel cell systems[J］.Chemical Engineering Science, 2012,67(1):15-25.

[16] HU Z,HAMEYER K.A method of constraint handling for speed-controlled induction machines[J］.IEEE Transactions on Industrial Electronics,2016,63(7):4061-4072.