An inertial group simulation method for a semi-physical simulation test of a launch vehicle
A semi-physical simulation and launch vehicle technology, applied in the field of semi-physical simulation of launch vehicle control systems, can solve the problems of increasing test costs
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[0099] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:
[0100] Such as figure 1 Shown is the schematic diagram of the inertial group simulator measuring dynamic characteristics of the present invention, figure 2 It is the principle diagram of the main functions of the inertial group simulator of the present invention, and the inertial group simulation method for the semi-physical simulation test of the launch vehicle of the present invention specifically includes the following steps:
[0101] Step (1), configure the parameters of the inertial group simulator according to the actual parameters of the simulated or measured inertial group, and the parameter configuration includes the installation matrix E g ,E a , the scaling factor K g 、K a , zero bias D g 、D a .
[0102] Step (2), collect externally sent attitude, speed and position information in each time period, and input the attitude, spee...
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