Science & Technology Review
|
2020, 38(21): 144-149
• Exclusive: System Engineering •
Longitudinal maneuverability optimization of flight control in autonomous carrier landing
Full
DONG Ran1, ZHANG Kunpeng2, WANG Xiaofeng1, WANG Lipeng3, LI Jiatong4
Affiliations
1. College of Information Engineering, Beijing Institute of Petrochemical Technology, Beijing 102617, China;
2. Aviation System Research Department, SERI, Beijing 100094, China;
3. College of Intelligent Systems Science and Engineering, Harbin Engineering University, Harbin 150001, China;
4. No. 704 Research Institute, China Shipping Industry Corporation, Shanghai 200031, China
Published: 2020-11-13
doi: 10.3981/j.issn.1000-7857.2020.21.018
Outline
Automatic carrier landing system (ACLS) permits high performance carrier-based aircraft to achieve autonomous safe and stable landing, thus its flight control system requires good maneuverability. In this paper, based on system stability theories, test data of F/A-18A fighter aircraft, and the response optimization tools of MATLAB, a novel parameter design method is proposed, and applied to optimizing the parameters of ACLS longitudinal flight control system in a loop by loop and from inside to outside manner. Simulation results show that the system with calibrated parameters has a better performance in responding to the command signal than that of F/A-18A aircraft.
automatic carrier landing
/
maneuverability
/
longitudinal control
/
test flight data
DONG Ran, ZHANG Kunpeng, WANG Xiaofeng, WANG Lipeng, LI Jiatong.
Longitudinal maneuverability optimization of flight control in autonomous carrier landing[J].
Science & Technology Review,
2020
, 38
(21)
: 144
-149
.
DOI: 10.3981/j.issn.1000-7857.2020.21.018
Year 2020 volume 38 Issue 21
PDF
492
122
Cite this Article
BibTeX
Article Info
doi: 10.3981/j.issn.1000-7857.2020.21.018
- Receive Date:2020-04-17
- Online Date:2020-11-17
- Published:2020-11-13