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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2021, Vol. 42 ›› Issue (3): 324301-324301.doi: 10.7527/S1000-6893.2020.24301

• Electronics and Electrical Engineering and Control • Previous Articles     Next Articles

Trajectory planning for parafoil system considering dynamic constraints in complicated environment

SUN Hao1, SUN Qinglin1, TENG Haishan2,3, ZHOU Peng2,3, CHEN Zengqiang1   

  1. 1. College of Artificial Intelligence, Nankai University, Tianjin 300350;
    2. Beijing Institute of Space Mechanics & Electricity, Beijing 100094;
    3. Laboratory of Aerospace Entry, Descent and Landing Technology, China Aerospace Science and Technology Corporation, Beijing 100094
  • Received:2020-05-27 Revised:2020-06-15 Published:2020-07-06
  • Supported by:
    The National Natural Science Foundation of China(61973172, 61973175,62003177); The Key Technologies Research and Development Program of Tianjin(19 JCZDJC32800); China Postdoctoral Science Foundation(2020M670633, 2020M670045)

Abstract: Because of the large inertia and strong nonlinearity of the parafoil system, the object trajectory based on the mass model cannot satisfy the dynamic constraints of the parafoil under complicated terrain conditions. Therefore, application of high-order dynamic models to trajectory planning becomes an inevitable trend in calculating a real system trajectory. However, the dynamic model of the parafoil is complicated. Currently, one of the urgent problems to be solved is to ensure smooth and stable trajectories. To overcome this difficulty, this study builds an accurate six degree-of-freedom dynamic model of the parafoil which is then introduced into the trajectory planning. A multi-stage trajectory planning strategy is designed by improving the Gauss pseudo-spectrum method based on segment point planning, initial discrete point planning and discrete point self-configuration. The simulation results show the effectiveness of the proposed algorithm in overcoming the difficulty of obtaining a stable trajectory with a dynamic model by the traditional planning method. Accurate terrain avoidance is realized under complex external conditions, and the planning trajectory can satisfy the dynamic constraints of the parafoil.

Key words: parafoil systems, dynamic constraints, trajectory planning, multiple constraints, complex terrain

CLC Number: