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Design and analysis of takeoff and landing control algorithm for four-rocket boosting drone

Authors :
TIAN Weili
YAN Zhaowu
LI Wen
JIA Dong
Source :
Hangkong gongcheng jinzhan, Vol 15, Iss 1, Pp 105-117 (2024)
Publication Year :
2024
Publisher :
Editorial Department of Advances in Aeronautical Science and Engineering, 2024.

Abstract

Fixed wing UAV takes off and lands on the ground with high requirements,which limits the application and development of fixed wing aircraft. Therefore,a scheme of four-rocket boosting drone to realize short-range takeoff and landing process is proposed,and the takeoff and landing control algorithm of rocket boosting drone is studied. In the process of research,the control strategy of rocket boosting drone takeoff and landing process is designed;The mathematical models of UAV aerodynamic force,booster rocket force,engine thrust and control law are established;The dynamic equation of the takeoff and landing process of UAV is constructed;A control algorithm based on PID control is designed to control the target UAV to complete the take-off and landing process safely and stably under various interference environments. MATLAB software is used for programming and simulation calculation. The simulation results show that the control algorithm and control law designed meet the control requirements of the target UAV during takeoff and landing.

Details

Language :
Chinese
ISSN :
16748190
Volume :
15
Issue :
1
Database :
Directory of Open Access Journals
Journal :
Hangkong gongcheng jinzhan
Publication Type :
Academic Journal
Accession number :
edsdoj.07b8060df5f4eac891726cf105bce75
Document Type :
article
Full Text :
https://doi.org/10.16615/j.cnki.1674-8190.2024.01.12