Xiaobao Han

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This paper puts forward a fuel control method for scramjet test. The control method of the Kholod scramjet flight test was analyzed systematically and regarding combustor surface pressure as the controlled parameter was verified by numerical simulations. The linear mathematical equations were established by system identification and the PID controller was(More)
Parameter estimation technologies play an important role in improving the performances of complex system control and health monitoring. To guarantee the global parameter estimation stability and robustness of aero-engine under the existence of disturbance, the new robust filter design and solving method for polynomial linear parameter varying (PLPV) model(More)
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