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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Bibliographic Details
Published in:Journal of physics. Conference series Vol. 1721; no. 1; pp. 12038 - 12047
Main Authors: Yang, Kai, Xu, Chen, Xu, Yan
Format: Journal Article
Language:English
Published: IOP Publishing 01.01.2021
ISSN:1742-6588, 1742-6596
Online Access:Get full text
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Summary: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