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State of art on energy management strategy for hybrid-powered unmanned aerial vehicle 被引量:13

State of art on energy management strategy for hybrid-powered unmanned aerial vehicle
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摘要 New energy sources such as solar energy and hydrogen energy have been applied to the Unmanned Aerial Vehicle(UAV), which could be formed as the hybrid power sources due to the requirement of miniaturization, lightweight, and environmental protection issue for UAV. Hybrid electrical propulsion technology has been used in UAV and it further enforces this trend for the evolution to the Hybrid-Powered System(HPS). In order to realize long endurance flight mission and improve the energy efficiency of UAV, many researching works are focused on the Energy Management Strategy(EMS) of the HPS with digital simulation, ground demonstration platforms and a few flight tests for the UAV in recent years. energy management strategy, in which off-line or on-line control algorithms acted as the core part, could optimize dynamic electrical power distribution further and directly affect the efficiency and fuel economy of hybrid-powered system onboard.In order to give the guideline for this emerging technology for UAV, this paper presents a review of the topic highlighting energy optimal management strategies of UAV. The characteristics of typical new energy sources applied in UAV are summarized firstly, and then the classification and analysis of the architecture for hybrid power systems in UAV are presented. In the context of new energy sources and configuration of energy system, a comprehensive comparison and analysis for the state of art of EMS are presented, and the various levels of complexity and accuracy of EMS are considered in terms of real time, computational burden and optimization performance based on the optimal control and operational modes of UAV. Finally, the tendency and challenges of energy management strategy applied to the UAV have been forecasted. New energy sources such as solar energy and hydrogen energy have been applied to the Unmanned Aerial Vehicle(UAV), which could be formed as the hybrid power sources due to the requirement of miniaturization, lightweight, and environmental protection issue for UAV. Hybrid electrical propulsion technology has been used in UAV and it further enforces this trend for the evolution to the Hybrid-Powered System(HPS). In order to realize long endurance flight mission and improve the energy efficiency of UAV, many researching works are focused on the Energy Management Strategy(EMS) of the HPS with digital simulation, ground demonstration platforms and a few flight tests for the UAV in recent years. energy management strategy, in which off-line or on-line control algorithms acted as the core part, could optimize dynamic electrical power distribution further and directly affect the efficiency and fuel economy of hybrid-powered system onboard.In order to give the guideline for this emerging technology for UAV, this paper presents a review of the topic highlighting energy optimal management strategies of UAV. The characteristics of typical new energy sources applied in UAV are summarized firstly, and then the classification and analysis of the architecture for hybrid power systems in UAV are presented. In the context of new energy sources and configuration of energy system, a comprehensive comparison and analysis for the state of art of EMS are presented, and the various levels of complexity and accuracy of EMS are considered in terms of real time, computational burden and optimization performance based on the optimal control and operational modes of UAV. Finally, the tendency and challenges of energy management strategy applied to the UAV have been forecasted.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第6期1488-1503,共16页 中国航空学报(英文版)
基金 upported by the Open Innovative Fund of Xi’an Aisheng Technology Group Company of China (No. ASN-IF2015-0202)
关键词 ENERGY management strategy(EMS) HYBRID power system(HPS) New ENERGY SOURCES Optimization algorithms UAV Energy management strategy(EMS) Hybrid power system(HPS) New energy sources Optimization algorithms UAV
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  • 1刘斌,马晓平,王和平,周康生.小型电动无人机总体参数设计方法研究[J].西北工业大学学报,2005,23(3):396-400. 被引量:31
  • 2邓海强,余雄庆.太阳能飞机的现状和发展趋势[J].航空科学技术,2006(1):28-30. 被引量:28
  • 3王冠林,武哲.垂直起降无人机总体方案分析及控制策略综合研究[J].飞机设计,2006,26(3):25-30. 被引量:30
  • 4ZHU X, GUO Z, HOU Z. Solar-powered airplanes: A historical perspective and future challenges[J]. Progress in Aerospace Sciences, 2014, 71: 36-53.
  • 5NOTH A. Design of solar powered airplanes for continu- ous flight[D]. Ztirich: ETH Ztirieh, 2008: 1-17.
  • 6SWIDER-LYONS K E, MACKRELL J A, RODGERS J A, et al. Hydrogen fuel cell propulsion for long endurance small UAVs[C]//Proceeding of the AIAA Centennial of Naval Aviation Forum " 100 Years of Achievement and Progress". Reston: AIAA, 2011:1 8.
  • 7LTD H E S P. Aerostak data sheet[M]. 2015: 1-3.
  • 8VERSTRAETE D, GONG A, LU D D C, et al. Experi- mental investigation of the role of the battery in the Aero- Stack hybrid, fuel-cell-based propulsion system for small unmanned aircraft systems[J]. International Journal of Hydrogen Energy, 2015, 40(3): 1598-1606.
  • 9VERSTRAETE D, LEHMKUEHLER K, GONG A, et al. Characterisation of a hybrid, fuel-cell-based propulsion system for small unmanned aircraft[J]. Journal of Power Sources, 2014, 250: 204-211.
  • 10NOLL T B J, PEREZ DAVIS M. Investigation of the He- lios Prototype Aircraft Mishap[R]. Washington, D. C. : NASA, 2004.

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