Longitudinal control and airwake suppression algorithm for carrier-based aircraft based on model predictive control

被引:2
作者
Tang, Ke [1 ]
Wang, Wei [1 ]
Meng, Yue [1 ]
Zhang, Mingyan [1 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Sch Instrument Sci & Optoelect Engn, Beijing, Peoples R China
来源
2018 EIGHTH INTERNATIONAL CONFERENCE ON INSTRUMENTATION AND MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC 2018) | 2018年
关键词
Carrier landing; Carrier airwake; Model predictive control; Flight control;
D O I
10.1109/IMCCC.2018.00249
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Compared with landing on a fixed runway, carrier landing faces with more difficulties and higher risk, such as shorter runway, pitching decks and high relative velocity. What's more, the carrier airwake further deteriorates the situation, which causes aircraft trajectory deviation from reference landing path, and the risk of waving off or colliding with the carrier. Carrier landing safety is therefore seriously affected. Aiming at this problem, on the basis of modelling the small-disturbance motion equation of a carrier-based aircraft under the landing status, the article presented a flight control and airwake rejection algorithm based on state space model predictive control(MPC), in which the airwake models were considered. The computer simulation experiments indicated that the proposed method could effectively suppress the disturbance of carrier airwake, and improve the landing accuracy significantly.
引用
收藏
页码:1200 / 1203
页数:4
相关论文
共 10 条
  • [1] [Anonymous], 1980, MILF8785C
  • [2] FROISY JB, 1994, COMPUT CHEM ENG, V33, P235
  • [3] Heffley R K, 1990, RHENAV90TR1 US DEP N
  • [4] J Deng, 2012, J SYSTEM SIMULATION
  • [5] Fuzzy modelling control for aircraft automatic landing system
    Juang, JG
    Chio, JZ
    [J]. INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, 2005, 36 (02) : 77 - 87
  • [6] Kouvaritakis B, 2016, ADV TXB CONTR SIG PR, P175, DOI 10.1007/978-3-319-24853-0_5
  • [7] Lind R, 2013, AIAA J
  • [8] Nelson RC., 1998, Flight Stability and Automatic Control, V2
  • [9] Q Zhu, 2013, J HARBIN ENG U
  • [10] Xia G, 2015, J AIRCRAFT, V53, P1