Triple Redundant arrangement full function and aviation grade flight control and navigation system, especially application for the higher reliability requirement of sensitive flight mission or highly valuable payloads.
Integration three autopilot systems for triple redundancy. If any one of the three systems fail, the remaining two take over flight control and navigation as double redundant arrangement.
Each autopilot unit is composed of processor, IMU, static/dynamic pressure sensor, magnetic sensor and GPS/ BeiDou module.
Each autopilot features independent positioning process, redundant management, fault detection and isolation and refactoring.
Feature three channel positioning control analysis, and real time sharing of three channels sensors data, parameters and output command.
Integrate high accuracy RTK BeiDou/GPS module, featuring centimeter level accuracy of UAV positioning.
Support additional higher performance IMU sensor, navigation devices, vertical gyroscope, magnetic heading sensor.
Built-in 96 Mbyte data recorder for 20h flight logging data recording.
Modular design embedded OS and MPC 5200 processor from Freescale, which make the autopilot secondary development availability based on its abundant CPU resources and data processing platform.
Support hardware-in-the-loop simulation based on the standard communication protocol.