Open AccessDesign and Implementation of Trajectory Planning Algorithm for UAV Borne Air-to-Surface Missile
Author(s) -
Kai Yang,
Xu Chen,
Yan Xu
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1721/1/012038
Subject(s) - missile , trajectory , missile guidance , range (aeronautics) , air to air missile , mode (computer interface) , aerospace engineering , guidance system , computer science , engineering , physics , astronomy , operating system
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.