Model Based Design and Procedure of Flight Control System for Unmanned Aerial Vehicle

被引：0

作者：

Wang, Kaiqiang ^{[1
]}

Gong, Zheng ^{[2
]}

Hou, Yanze ^{[1
]}

Zhang, Minjie ^{[1
]}

Liu, Changxiu ^{[1
]}

Chen, Runfeng ^{[1
]}

机构：

[1] China Acad Space Technol, Inst Manned Space Syst Engn, Beijing, Peoples R China

[2] Nanjing Univ Aeronaut & Astronaut, Coll Aerosp Engn, Nanjing, Peoples R China

来源：

PROCEEDINGS OF 2020 3RD INTERNATIONAL CONFERENCE ON UNMANNED SYSTEMS (ICUS) | 2020年

关键词：

model-based design; flight control system; unmanned aerial vehicle; test and validation;

D O I：

10.1109/icus50048.2020.9274980

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Model-hased design (MBD) is an efficient systematic approach for complex system design. It uses models for information transfer and interaction among the designers and engineers. With the use of MBD, communication accuracy and quality are enhanced, a large sum of iterative manual work is saved, and the system design efficiency can he improved. This paper presents practical design and procedure of flight control system for unmanned aerial vehicle (UAV). The basic design contents and procedure of flight control system based on MBD are illustrated first. Then, the system model as well as the constitutional modules for MBD are established and presented. On the basis of the model, the flight software or the C code is generated automatically, and the system validation through X-In-the-Loop (XIL) tests is carried out. The model used in each step of XIL tests is also introduced. Finally, a test case is given as an example.

引用

页码：763 / 768

页数：6

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