基于DSP+FPGA的激光半主动导弹飞控软件设计

Design of Flight control Software for Laser Semi-active Guided Missile Based on DSP+FPGA

摘要:

为满足弹载飞控软件实时性、可靠性的要求,设计了基于DSP+FPGA硬件结构的某型号激光半主动导弹飞控软件,其中TMS320C6713 DSP作为主处理器,FPGA作为协处理器,两者进行高度并行数据处理。飞控软件包括测试模式和正常工作模式,测试模式完成弹上设备的测试和维护,正常模式完成导弹的发射和控制。本着高内聚、低耦合原则,对飞控软件采用模块化设计方法,给出了模块组成、模块功能以及模块间的关系。最后给出了飞控软件半实物仿真试验结果及改进方向。

Abstract:

In order to meet the requirements of real-time and reliability of missile-borne flight control software, a laser semi-active guided missile flight control software based on the hardware structure of DSP+ FPGA is designed.Themain processor is TMS320 C6713 DSP and the coprocessor is FPGA, Both of them process data parallely.Flight control software includes test mode and normal mode.Test mode completes the test and maintenance of missile equipments and normal mode completes the launch and control of missile. Based on the principle of high cohesion and low coupling, modularized design method is adopted for flight control software.Module composition, module function and the relationship between the modules are given.Finally, the results of the hardware-in-the-loop simulation and the improvement direction are given.