This paper represents a new interconnected architecture of Flight control System (FCS). It can solve the problems of massive equipment and large cross link information. The interconnected architecture adopts double CAN-Bus to construct a redundant flight control systematic bus. This paper will illustrate the characters of double CAN-Bus comparing with the characters of CAN-Bus firstly. Then it will present the bus controller hardware design, allowance design, network communication protocol, software flow and code design respectively. The experimental results show that the bus is running well, can satisfy the small vehicle control system of a high real time capability and node demand, at the same time system has high reliability, open etc.
Design of Flight Control System Bus Controller of UAV Based on Double CAN-Bus
Applied Mechanics and Materials ; 479-480 ; 641-645
2013-12-06
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Robust controller design for self-repairing flight control system
British Library Online Contents | 1996
|Controller design for a digital flight control system DFCS
Tema Archiv | 2009
|FLIGHT DEVICE, FLIGHT CONTROLLER AND FLIGHT CONTROL METHOD
Europäisches Patentamt | 2018
|Active Control Technology and Restructurable Flight Controller Design
British Library Conference Proceedings | 1999
|