Receding Horizon Trajectory Generation of Stratospheric Airship in Low-Altitude Return Phase

Receding Horizon Trajectory Generation of Stratospheric Airship in Low-Altitude Return Phase

The contribution of this paper is the proposal of a new receding horizon trajectory generation method for stratospheric airships’ return phase. Since the energy consumption, wind field and path constraints are restrictions during the return phase of airships at low altitude, it is crucial to develop...

Täydet tiedot

Bibliografiset tiedot
Päätekijät: Yuhao Jing, Yang Wu, Jiwei Tang, Pingfang Zhou, Dengping Duan
Aineistotyyppi: Artikkeli
Kieli:English
Julkaistu: MDPI AG 2022-10-01
Sarja:Aerospace
Aiheet:
stratospheric airships return phase
trajectory generation
optimal numerical solution
path constraints
environmental constraints
Linkit:https://www.mdpi.com/2226-4310/9/11/670

Internet

https://www.mdpi.com/2226-4310/9/11/670

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