Influence of maneuvering modes on flared landing performance of parafoil system

CHENG Yang; QIU Bowen; YU Li; LI Yanjun; CAO Haoran

doi:10.13700/j.bh.1001-5965.2022.0914

Volume 50 Issue 12

Dec. 2024

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Journal of Beijing University of Aeronautics and Astronautics > 2024 > 50(12): 3940-3946.

CHENG Y，QIU B W，YU L，et al. Influence of maneuvering modes on flared landing performance of parafoil system[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3940-3946 （in Chinese） doi: 10.13700/j.bh.1001-5965.2022.0914

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Influence of maneuvering modes on flared landing performance of parafoil system

doi: 10.13700/j.bh.1001-5965.2022.0914

CHENG Yang¹,
QIU Bowen¹,
YU Li^{1, 2
,
,},
LI Yanjun^{1, 2},
CAO Haoran¹

1.
Key Laboratory of Aircraft Environment Control and Life Support，Ministry of Industry and Information Technology，Nanjing University of Aeronautics and Astronautics，Nanjing 210016，China
2.
College of Aerospace Engineering，Nanjing University of Aeronautics and Astronautics，Nanjing 210016，China

Funds: National Natural Science Foundation of China (11972192)

More Information

Corresponding author: E-mail：yuli_happy@163.com
Received Date: 10 Nov 2022
Accepted Date: 19 Dec 2022

Available Online: 06 Jan 2023

Publish Date: 03 Jan 2023

Abstract

Abstract

A two-body 9-degree of freedom (DOF) dynamics model of the parafoil system was established, and the Runge-Kutta method was used for dynamic programming calculation. The numerical results of the system velocities and parafoil and load attitudes were consistent with the results in the literature, and the maximum error was 8.2%. On this basis, the influence of hierarchical maneuvering and maneuvering velocity on the flared landing performance of the parafoil system was investigated. The variations of minimum horizontal velocity, minimum vertical velocity, and maximum angle of attack of parafoil were obtained. The results show that the flared landing performance under one-time maneuvering is better than that under hierarchical maneuvering. If the maneuvering duration is too long or too short, the vertical velocity will increase. Both maneuverings featuring first accelerating and then decelerating and constant velocity can ensure good flared landing performance. The minimum vertical velocity and the flight stability of the parafoil should both be considered in the selection of the maneuvering velocity.
- parafoil,
- flared landing performance,
- 9-DOF model,
- maneuvering modes,
- maneuvering velocity

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References(20)

References

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