Keywords: unmanned aerial vehicle, landing gear control system, signal time delays, dynamic systems modeling, electronic part of the control system, software environment
Analysis of the impact of time delays on the operation of the chassis control system of an unmanned aerial vehicle
UDC 629.735
DOI: 10.26102/2310-6018/2025.51.4.044
The relevance of this research stems from the need to improve the reliability and safety of unmanned aerial vehicle landing gear control systems operating under conditions of time delays in control signal transmission. Such delays, which occur during the measurement, processing, and execution of commands, significantly impact the system's response time and can lead to failures during landing. Therefore, this study aims to model the behavior of the electronic component of an unmanned aerial vehicle landing gear control system, taking into account the cumulative time delays that determine the overall response time. The primary research method is numerical simulation in the time domain, performed in the Simintech software environment, which enabled the implementation of a structural block model of signal transmission from the position sensor to the actuator. The results showed that the total system delay is approximately two seconds for an acceptable body tilt angle of no more than fifteen degrees. If this value is exceeded, the control signal is not generated, providing additional protection against emergency conditions. The obtained results confirm the need to optimize the control system architecture and select faster-responding components. The research materials are of practical value for the design and analysis of control systems for aircraft-type unmanned aerial vehicles.
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Keywords: unmanned aerial vehicle, landing gear control system, signal time delays, dynamic systems modeling, electronic part of the control system, software environment
For citation: Khasanov I., Berezhansky N., Akaemov P. Analysis of the impact of time delays on the operation of the chassis control system of an unmanned aerial vehicle. Modeling, Optimization and Information Technology. 2025;13(4). URL: https://moitvivt.ru/ru/journal/pdf?id=2096 DOI: 10.26102/2310-6018/2025.51.4.044 (In Russ).
Received 07.10.2025
Revised 14.11.2025
Accepted 20.11.2025