Abstract:Over the last three decades,the growing demand for safety,reliability,maintainability,and miniaturization in small unmanned aerial vehicle (UAV) has motivated significant research in new technology. A dual redundant fault tolerant flight control platform is designed based on the technology of system on a programmable chip (SOPC) and the fault-tolerant technology. The implementation scheme about hardware and software of fault-tolerant system is given in detail. The key technology about the synchronization technology,fault diagnosis and location,dynamic reconfiguration and isolation is studied in detail. After lots of simulations and experiments,it shows that the design scheme is reasonable. The platform not only realizes the basic function of the flight control,but also has a high level of integration and flexibility,and can keep safe after a failure.