![]() ![]() It provides signal interfaces from other parts of the system and from the system to the on-board cross-link equipment on the machine and process the signals. Flight control computer is also the management part of all the system, which is responsible for redundancy management calculation, logical judgment, working mode conversion, and achieves the declaration of system state, fault alarm and BIT function of the whole flight control system. Providing power supply for some other external partsįlight control computer, the core of the UAV flight control system, is the solution device of control system to realize the control law calculation function of flight control system and output control command to servo system.Self-test capability to meet the system testability requirements and providing test circuits for other parts.According to the information of command sensor and flight movement sensor, it performs control law calculation and the result is input to servo system to control motion of rudder actuator.Achieving redundancy management and self-test function through hardware and software to meet the reliability requirements of flight computer and flight control system reliable.Laboratory automation, research and design verification 5﹪~95﹪, no condensationĮxternal dimensions (L×W×H) (without ear). It is a flight control computer which integrates aviation control with task to meet the autonomous flight control and mission of the multi-rotatable wings/fixed-wings airplane and helicopter. The whole machine frame structure is designed by aviation aluminum alloy-alloy so it has obvious characters of firm construction and light body. This device contains one port of RS232 and one port of RS422, debug interface for JTAG and UART, built-in inertial navigation, barometer, GPS module and a base with JPMZ-0.5 shock absorber. It adopts PC104 stack, peripheral module construction realized by external extend device’s local bus of embedded processer. The device is a flight control computer platform applied to UAV with laminated structure of four layers inside, including functions as data processing, data acquisition, communication, long-distance data transmission, direction inertial navigation and so on. PC104 stack structure with ATAG & UART test interfaces.The base with a JPMZ-0.5 shock absorber.Provide DC 24Voltage output and motor driving module.Embedded inertial navigation unit, differential GPS unit.Make flight operations more energy efficient and safer. And the safety warning is displayed in the APP to help adjust the adaptability of all aspects of the fuselage device. K++V2 comes with intelligent vibration analysis function, which can judge the vibration of the aircraft in real time. Main control supports backup power interface Reduce the investment in after-sales maintenance The aging of the frame can also fly stable Responding to various complex vibration effects The trajectory is more precise and the flight is smoother The vertical control accuracy is increased by 20% ![]() ![]() The flight accuracy of the route is increased by 25% As a new generation flagship flight controller system, K++V2 integrates the advantages of the classic flight controller K3A, and strengthens compatibility and multiple redundancy schemes to form a redundant redundant control system with superior performance, strong reliability and effective guarantee Work safety ![]()
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