A measurement and control system and method suitable for high dynamic uncontrolled return of aircraft separation body
A technology of measurement and control system and aircraft, applied in the direction of weapon types, offensive equipment, projectiles, etc., can solve problems such as environmental pollution, personnel injury, and large spread of booster landing points, so as to reduce the range of landing areas and improve safety Effect
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[0060] Such as figure 1 As shown, the specific components of the measurement and control system include power supply module, MEMS inertial measurement module, satellite navigation receiving module, control module, radio frequency transmission module, image measurement module, data storage module, digital input and output module, and switch input and output module. Partial composition. The specific implementation is:
[0061] 1) Complete the parameter collection and information fusion of the MEMS inertial measurement module and the satellite navigation receiving module during the flight;
[0062] 2) Receive status information such as take-off signals and aircraft separation signals, and control the power supply module to supply power to the separation pyrotechnics according to the predetermined time;
[0063] 3) Complete the function of collecting and storing digital image signals;
[0064] 4) Send positioning and attitude information to other subsystems through RS-485 or RS...
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