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According to the safety and reliable transmission and integration requirement of co-guidance information for autonomous aero craft flying formation, the control mode of autonomous flying formation was studied. The paper firstly presents the AdHoc-based communication network scheme of autonomous flying formation, and the design and implementation mechanism of four-level networking protocol stack model...
The applications of plug and play (PnP) method to flying control computer for aerospace launch vehicle is studied, and the plug-and-play model of flying control computer is discussed. Then the PnP design scheme of flying control computer is presented, also the validation experiment is carried through. At last, a simple demonstration system is built, and the research method is tested and analyzed,...
This paper proposed an automatic detection and automatic configuration method of 1553B RT device based on SoC chip. This method made SoC as information dealing unit of each terminal on 1553 bus. Electronic data form was added on the RT device, and a multi-task management procedure was run on the BC device. When a RT device was plugged in or pulled out the 1553 bus, the operation was detected and the...
This paper introduces a kind of reconfigurable interface realized with the Dynamic Reconfigurable FPGA. The interface can automatically switch its control circuit according to the interface type of external sensor device. Thereby, the interface is compatible to various interfaces. In addition, the interface can help control device of aero craft to detect external sensor device, this is good for establishing...
Aiming at the developing requirements on rapid integration of control system for responsive aerospace launch vehicle, this paper put forward a kind of architecture of plug-and-play/PnP control system, and presents the generic model of plug-and-play control system for aerospace launch vehicle and the standardization communication machenism. Then the principle validation experiment is carried through...
Flying control system is the core fabrication division of aircraft", "and its working reliability and the performance sticking up to strong electromagnetic pulse(SEMP) can directly affect the success or fail of flying mission. Aiming at the protecting problems of flying control system under strong electromagnetic pulse environment, injury effect and latent threat to aircraft as well as hurt...
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