Paper
16 August 2024 Architecture design of four redundant flight control system
Author Affiliations +
Proceedings Volume 13218, First Aerospace Frontiers Conference (AFC 2024); 1321804 (2024) https://doi.org/10.1117/12.3032393
Event: First Aerospace Frontiers Conference (AFC 2024), 2024, Xi’an, China
Abstract
Redundant flight control systems typically have high flexibility and customizability, suitable for different types of high-value drones. This article proposes a new architecture for a four degree redundant flight control system, which is based on the traditional four degree redundant flight control system architecture. By adding a CANFD bus to achieve signal interaction between flight control computers, the resulting voting values can be used as a reference for signal arbitration in the next cycle. This design can increase the reliability of the redundancy system and solve the problem of inability to distinguish faults when the signal voting is 2:2 in traditional designs. Finally, using the proposed method, a redundant flight control system was developed for a certain experimental drone, and its effectiveness was successfully verified through ground semi physical experimental testing.
(2024) Published by SPIE. Downloading of the abstract is permitted for personal use only.
Tianyi Xie, Wenya Zhou, Qinghua Zeng, Dali Zhang, and Mingtao Cao "Architecture design of four redundant flight control system", Proc. SPIE 13218, First Aerospace Frontiers Conference (AFC 2024), 1321804 (16 August 2024); https://doi.org/10.1117/12.3032393
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KEYWORDS
Sensors

Control systems

Computing systems

Reliability

Tolerancing

Control systems design

Design

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