Design and Implementation of Trajectory Planning Algorithm for UAV Borne Air-to-Surface Missile

This paper firstly introduces the development of domestic UAV borne air-to-ground missile guidance control systems and summarizes the current and ongoing research on the trajectory design of airborne missiles for unmanned aerial vehicles. Secondly, it introduces the traditional single-mode guided un...

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Veröffentlicht in:	Journal of physics. Conference series Jg. 1721; H. 1; S. 12038 - 12047
Hauptverfasser:	Yang, Kai, Xu, Chen, Xu, Yan
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	IOP Publishing 01.01.2021
ISSN:	1742-6588, 1742-6596
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	This paper firstly introduces the development of domestic UAV borne air-to-ground missile guidance control systems and summarizes the current and ongoing research on the trajectory design of airborne missiles for unmanned aerial vehicles. Secondly, it introduces the traditional single-mode guided unmanned aerial vehicle air-to-ground missile trajectory design schemes and the new trajectory planning schemes for multi-mode compound guidance unmanned aerial vehicle borne air-to-ground missile. Finally, through mathematical simulation, it shows the characteristics of different trajectory schemes in terms of range, relative launch altitude and off-boresight capability.
ISSN:	1742-6588 1742-6596
DOI:	10.1088/1742-6596/1721/1/012038