Design and Implementation of a Launch Control Computer Based on DSP
Liu Shuo;Lu Hao;Gao Hao;Aeronautical Computing Technique Research Institute,AVIC;School of Computer Science,Northwestern Polytechnical University;
For the aircraft developed with independent airborne missiles, it is necessary to control the conversion of the launcher to meet the requirements of GJB1188 A in order to achieve the aircraft and missile electrical interface between the unity. In order to meet the requirements of missile launcher control system, a hardware and software design and implementation method of DSP-based launch control computer is proposed, and the conversion of data and control signals between aircraft and missile is completed. The launch control computer is stable and reliable, and meets the requirements of the launcher control system. Design is not only used for a kind of airborne missile launchers, for non-standard aircraft hangings have universal reference.
【CateGory Index】： TJ768;V271.4