Energy optimized maneuver trajectory generation for unmanned aerial vehicles

被引:0
作者
Yang S. [1 ]
Zhang X. [1 ]
机构
[1] Key Laboratory, AVIC Xi'an Flight Automatic Control Research Institute, Xi'an
来源
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2020年 / 41卷
关键词
Energy optimization; Maneuver; Pull-up turn; Trajectory generation; Unmanned Aerial Vehicles (UAVs);
D O I
10.7527/S1000-6893.2020.24288
中图分类号
学科分类号
摘要
Energy of motion for maneuver flight of unmanned aerial vehicles (UAVs) based on energy optimization enables the UAVs to gain energy superiority without losing decisive position superiority. Adequate energy superiority can be translated into effective position superiority, facilitating the UAVs in changing into other maneuver from current maneuver at any moment, which is crucial for UAVs to win the aerial combat. This paper examines the maneuver trajectory generation methods for UAVs based on energy optimization, designs appropriate maneuver commands in the UAV flight envelope to achieve optimal energy performance, and uses detailed pull-up turn maneuver trajectory commands as an example. In addition, a comparison is made with the classical maneuver trajectory method. Results show that with the designed method, the time consumption of maneuver flight is shortened by 28.6% to 83.8%, and the energy undulate quantity of the UAV is reduced by 64.7% to 70.1%, thereby realizing energy optimization for UAV maneuver flight. © 2020, Beihang University Aerospace Knowledge Press. All right reserved.
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  • [1] ZHANG X L, YANG Q W., Research on real time trajectory generation based on tactical maneuvers data base, Flight Dynamics, 26, 3, pp. 29-32, (2008)
  • [2] LIU P, WANG W J, CHEN X, Et al., Air combat maneuvering flight trajectory generation and control, Qrdnance Industry Automation, 37, 11, pp. 76-80, (2018)
  • [3] DING D L, WANG J, DONG K S, Et al., Rapid generation method of UCAV tactical maneuver trajectory based on RBF network, Systems Engineering and Electronics, 41, 1, pp. 96-104, (2019)
  • [4] WANG J, DING D L, DONG K S, Et al., UCAV autonomous air combat tactical maneuvering modeling and trajectory generation, Fire Control & Command Control, 43, 12, pp. 45-49, (2018)
  • [5] CHEN Y L., Optimal design of post stall maneuverable trajectory based on nonlinear programming method, Journal of Nanjing University of Aeronautics & Astronautic, 45, 6, pp. 746-751, (2013)
  • [6] WANG X P, LIN Q Y, DONG X M., Aircraft evasive maneuver trajectory optimization based on QPSO, 2010 Intenational Congress Congress on Ultra Modern Telecommunications and Control Systems and Workshops, pp. 416-420, (2010)
  • [7] HURST A, WICKENHEISER A, GARCIA E., Localization and perching maneuver tracking for a morphing UAV, 2008 IEEE/ION Position, Location and Navigation Symposium, pp. 1238-1245, (2008)
  • [8] RAO D V, TANG H, GO T H., A parametric study of fixed-wing aircraft perching maneuvers, Aerospace Science and Technology, 42, pp. 459-469, (2015)
  • [9] ZHU J W, LIU L H, TANG G J, Et al., Optimal diving maneuver strategy considering guidance accuracy for hypersonic vehicle, Acta Astronautica, 4, 1, pp. 231-242, (2014)
  • [10] KONSTANTINOV M S, ORLOV A A., Optimization of the transfer trajectory of a low thrust spacecraft for research of jupiter using an earth gravity-assist maneuver, Solar System Research, 48, 7, pp. 606-612, (2014)