Trajectory planning of stratospheric airship for station-keeping mission based on improved rapidly exploring random tree

被引:11
作者
Luo, Qin-chuan [1 ]
Sun, Kang-wen [1 ]
Chen, Tian [2 ]
Zhang, Yi-fei [3 ]
Zheng, Ze-wei [4 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Inst Unmanned Syst, Beijing 100191, Peoples R China
[3] Beihang Univ, Sch Elect & Informat Engn, Beijing 100191, Peoples R China
[4] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Stratospheric airship; Trajectory planning; Wind potential energy; Location potential energy; Rapidly exploring random tree(RRT); ALTITUDE; SIMULATION;
D O I
10.1016/j.asr.2023.10.002
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The station-keeping mission is one of the common missions of stratospheric airships. Its movement is sensitive to wind due to the large size and low airspeed of stratospheric airships. When the wind speed exceeds the maximum airspeed of the airship, the airship may fly out of the given mission region. Therefore, station-keeping trajectory planning is a new trajectory planning problem that has never existed before. A rapidly exploring random tree algorithm for station-keeping(RRT-SK) is proposed to solve the trajectory planning problem under multiple constraints of the airship, and an artificial potential field method (APF) considering wind field and relative position is designed as the objective function of the RRT-SK algorithm, both of which form the RRT-SK strategy used for the stratospheric airship station-keeping trajectory planning under multiple constraints. A multidisciplinary model is developed to simulate multiple constraints on the airship flight, including the energy model, thermal model, propulsion model, and kinematic model. The performance of the RRT-SK strategy is demonstrated in this multidisciplinary model with real wind fields. The results show that the multi-constrained station-keeping problem can be solved by the RRT-SK strategy. Compared with the conventional strategy, the RRT-SK strategy can improve the success rate of the airship's 24-h stationing flight and well cope with the impact of wind field changes and stationing area changes. Moreover, the RRT-SK strategy has better advantages in actual long-duration use. (c) 2023 COSPAR. Published by Elsevier B.V. All rights reserved.
引用
收藏
页码:992 / 1005
页数:14
相关论文
共 33 条
[1]   Path planning techniques for unmanned aerial vehicles: A review, solutions, and challenges [J].
Aggarwal, Shubhani ;
Kumar, Neeraj .
COMPUTER COMMUNICATIONS, 2020, 149 :270-299
[2]   High Altitude Airship: A Review of Thermal Analyses and Design Approaches [J].
Alam, Mohammad Irfan ;
Pasha, Amjad Ali ;
Jameel, Abdul Gani Abdul ;
Ahmed, Usama .
ARCHIVES OF COMPUTATIONAL METHODS IN ENGINEERING, 2023, 30 (03) :2289-2339
[3]  
An H., 2021, 2021 4 INT C ADV ELE
[4]   Optimal Path Planning Method for IMU System-Level Calibration Based on Improved Dijkstra's Algorithm [J].
Bai, Xuesong ;
Wang, Lu ;
Hu, Yuanbiao ;
Li, Pingfei ;
Zu, Yutong .
IEEE ACCESS, 2023, 11 :11364-11376
[5]   Autonomous navigation of stratospheric balloons using reinforcement learning [J].
Bellemare, Marc G. ;
Candido, Salvatore ;
Castro, Pablo Samuel ;
Gong, Jun ;
Machado, Marlos C. ;
Moitra, Subhodeep ;
Ponda, Sameera S. ;
Wang, Ziyu .
NATURE, 2020, 588 (7836) :77-+
[6]  
Colozza Anthony., 2003, Initial Feasibility Assessment of a High Altitude Long Endurance Airship
[7]   High-Altitude Platforms - Present Situation and Technology Trends [J].
d'Oliveira, Flavio Araripe ;
Lourenco de Melo, Francisco Cristovao ;
Devezas, Tessaleno Campos .
JOURNAL OF AEROSPACE TECHNOLOGY AND MANAGEMENT, 2016, 8 (03) :249-262
[8]   Performance simulation of high altitude scientific balloons [J].
Dai, Qiumin ;
Fang, Xiande ;
Li, Xiaojian ;
Tian, Lili .
ADVANCES IN SPACE RESEARCH, 2012, 49 (06) :1045-1052
[9]   Energy management strategy design and station-keeping strategy optimization for high altitude balloon with altitude control system [J].
Du, Huafei ;
Lv, Mingyun ;
Zhang, Lanchuan ;
Zhu, Weiyu ;
Wu, Yifei ;
Li, Jun .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 93
[10]   Station-keeping performance analysis for high altitude balloon with altitude control system [J].
Du, Huafei ;
Lv, Mingyun ;
Li, Jun ;
Zhu, Weiyu ;
Zhang, Lanchuan ;
Wu, Yifei .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 92 :644-652