This paper presents the composition, operating principle, and test method of an advanced dynamic test platform used in infrared air-to-air missile guidance and control system. Then the key techniques including real time distributed simulation, SBS High-Speed Broadcast Reflective Memory, and design of simulation software are discussed in detail. For dynamic test, the combination of numerical real time and hardware-in-the-loop simulation technique for each guidance and control component is expatiated.
Under the influence of various factors during production,К_Φ,the influence of Φ on guidance information coupling, is often out of tolerance. This has become a bottle-neck problem for the fabrication and adjustment of a certain infrared air-to-air missile seeker.
The generation way of pulse signal in IR seeker is important to control signal of Air to Air Missile(AAM). Based on signal generating principle of a certain type of IR AAM seeker,the authors compiled a simulating program for target image-point scanning with Visual C++ language and object-oriented technology,and made a simulation on computer for the processes of image-point scanning and pulse signal generating.