Path tracking control of solar-powered UAV based on energy management strategy

Q3 Engineering 西北工业大学学报 Pub Date : 2023-04-01 DOI:10.1051/jnwpu/20234120409
Lin Guo, Fei Liu, Jiayu Li, Pei He, Qingdong Li, Jiwei Wang, Yangming Guo
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Abstract

To coordinate the conflict between the high-altitude task and long-term energy efficiency of high-altitude long endurance solar UAV, it is one of the core issues of UAV control. A strategy combining the energy management with the route tracking is presented. Firstly, based on the three-dimensional particle motion model, energy storage battery model and solar energy acquisition model for the solar UAV, according to the aerodynamic parameters of the solar UAV and the typical horizontal flight, climb, descent and other motion processes of the solar UAV, the energy management strategy of the solar UAV is designed, and the allocation mechanism and optimal flight parameters of the energy acquisition, storage and consumption of the solar UAV in different flight stages are determined. The surplus solar energy is stored by using the gravitational potential energy, and then the energy management based on height adjustment is carried out to realize the longitudinal tracking control of the solar UAV under different lighting and energy conditions. Then based on the task requirements of the lateral movement of the solar UAV, a track tracking control method based on the feedback linearization method is established by decoupling the particle dynamics equation of the solar UAV, and the track tracking control of the solar UAV in the lateral direction is realized. Finally, a simulation throughout 24 hours is implemented and illustrated the effectiveness of the energy management strategy and route tracking control law.
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基于能量管理策略的太阳能无人机路径跟踪控制
协调高空长航时太阳能无人机的高空任务与长期能效之间的冲突,是无人机控制的核心问题之一。提出了一种将能量管理与路径跟踪相结合的策略。首先,基于太阳能无人机的三维粒子运动模型、储能电池模型和太阳能获取模型,根据太阳能无人机空气动力学参数和太阳能无人机典型的水平飞行、爬升、下降等运动过程,设计了太阳能无人机能量管理策略,确定了太阳能无人机在不同飞行阶段的能量获取、储存和消耗的分配机制和最佳飞行参数。利用重力势能储存剩余的太阳能,然后进行基于高度调节的能量管理,实现太阳能无人机在不同照明和能量条件下的纵向跟踪控制。然后,根据太阳能无人机横向运动的任务要求,通过解耦太阳能无人机的粒子动力学方程,建立了基于反馈线性化方法的轨迹跟踪控制方法,实现了太阳能无人机在横向方向上的轨迹跟踪控制。最后,通过24小时的仿真验证了能量管理策略和路径跟踪控制律的有效性。
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来源期刊
西北工业大学学报
西北工业大学学报 Engineering-Engineering (all)
CiteScore
1.30
自引率
0.00%
发文量
6201
审稿时长
12 weeks
期刊介绍:
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