Worst-Case Analysis of Complex Nonlinear Flight Control Designs Using Deep Q-Learning

被引:7
作者
Braun, David [1 ]
Marb, Michael M. [1 ]
Angelov, Jorg [1 ]
Wechner, Maximilian [1 ]
Holzapfel, Florian [1 ]
机构
[1] Tech Univ Munich, Inst Flight Syst Dynam, D-85748 Garching, Germany
关键词
Aircraft Flight Control System; Flight Control Law; Reinforcement Learning; Software Testing; Artificial Intelligence; VTOL Testing;
D O I
10.2514/1.G007335
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
With the objective of exposing hidden design deficiencies in complex nonlinear systems, this paper presents the use of reinforcement learning techniques for application in flight control law development and testing. Following the idea of worst-case testing, a deep Q-network agent is trained to identify input sequences that lead to detrimental system behavior. Because the analysis is based directly on the repeated interaction between the agent and the investigated system, no model simplifications are required, making the presented method applicable to highly complex systems. The capability of the learning-based worst-case analysis is demonstrated for the speed protection function of the hover flight control law of an electric vertical takeoff and landing (eVTOL) aircraft. The analysis discovers possible piloted maneuvers that violate the implemented protection algorithm. A root cause analysis of the emerging behavior reveals the neglect of an important flight mechanical coupling term in the design of the protection algorithm and ultimately leads to the revision and improvement of the controller. This demonstrates the benefits of the presented testing method for the design, verification, and validation of complex systems. The application to a high-fidelity system used for control law development of an actual eVTOL prototype currently under construction demonstrates the relevance of the method beyond academia.
引用
收藏
页码:1365 / 1377
页数:13
相关论文
共 40 条
[1]  
Akkinapalli V. S., 2018 AIAA GUID NAV C, DOI 10.2514/6.2018-1345
[2]  
Angelov J., 2021, DTSCH LUFTUND RAUMFA, DOI [10.25967/550011, DOI 10.25967/550011]
[3]  
[Anonymous], 2020, Transitioning to Electric Vertical Takeoff and Landing (EVTOL) and Other Aircraft Equipped for Simplified Vehicle Operations
[4]  
[Anonymous], 2021, STUDY SOCIAL ACCEPTA
[5]  
[Anonymous], 2021, 2 PUBLICATION PROPOS
[6]  
[Anonymous], 2000, Aeronautical Design Standard Performance Specification Handling Qualities Requirements For Military Rotorcraft, AMCOM ADS-33C
[7]  
Bhardwaj P., 2019, AIAA AV 2019 FOR, DOI 10.2514/6.2019- 3266
[8]  
Bhardwaj P., 2019, AIAA SCIT 2019 FOR, DOI 10.2514/6.2019-1923
[9]  
Bhardwaj P., 2018, 2018 APPL AER C, DOI 10.2514/6.2018-3479
[10]  
Bhardwaj P., 2021, AIAA SCIT 2021 FOR, DOI 10.2514/6.2021-1130