Analysis of Disturbance Characteristics of UAV Fuel Thermal Management System
Analysis of Disturbance Characteristics of UAV Fuel Thermal Management System
- Author(s): Wang Siqi ; Chen Wei Jian ; Chen Liuzhong
- DOI: 10.1049/cp.2018.0205
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- Author(s): Wang Siqi ; Chen Wei Jian ; Chen Liuzhong Source: CSAA/IET International Conference on Aircraft Utility Systems (AUS 2018), 2018 page (6 pp.)
- Conference: CSAA/IET International Conference on Aircraft Utility Systems (AUS 2018)
- DOI: 10.1049/cp.2018.0205
- ISBN: 978-1-78561-791-1
- Location: Guiyang, China
- Conference date: 19-22 June 2018
- Format: PDF
Based on the simplified airborne integrated thermal management system, this paper aims to study the dynamic characteristics of the system under the action of disturbance and provide theoretical basis for the study of system control scheme. This paper uses MATLAB/SIMULINK platform to develop Unmanned Aerial Vehicle (UAV) fuel system simulation model library. On the basis of the fuel of a certain UAV thermal management system, the simulation model is built and the simulation calculation of dynamic performance is carried on. Fuel temperature and the electronic equipment heat load is studied on the impact of change on system disturbance characteristics, and the control strategy of general application is put forward.
Inspec keywords: temperature control; autonomous aerial vehicles; aerospace engineering; aircraft power systems; fuel systems; digital simulation
Subjects: Aerospace control; Mobile robots; Telerobotics; Aerospace engineering computing; Transportation; Thermal variables control
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