Landing Point Control Technology of Parafoil System Based on Sliding Mode Control in a Complex Environment
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-6882-4_43
Reference6 articles.
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2. Carter, D., Singh, L., Wholey, L.: Band-limited guidance and control of large parafoils. In: 20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar, p. 2981 (2009). https://doi.org/10.2514/6.2009-2981
3. Leon, B.L., Wachlin, J., Ward, M.B.: A complete in-canopy system for autonomous aerial delivery. In: AIAA Aviation 2019 Forum, p. 3282 (2019). https://doi.org/10.2514/6.2019-3282
4. Tanaka, K., Tanaka, M., Iwase, A., Wang, H.O.: A rational polynomial tracking control approach to a common system representation for unmanned aerial vehicles. IEEE/ASME Trans. Mechatron. 25(2), 919–930 (2020). https://doi.org/10.1109/TMECH.2020.2965576
5. Moriyoshi, T., Yamada, K., Nishida, H.: The effect of rigging angle on longitudinal direction motion of parafoil-type vehicle: basic stability analysis and wind tunnel test. Int. J. Aerosp. Eng. 2020, 1–16 (2020). https://doi.org/10.1109/TMECH.2020.2965576
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