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Pitch attitude stabilization system utilizing engine pressure ratio feedback signals
Pitch attitude stabilization system utilizing engine pressure ratio feedback signals
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机译:利用发动机压力比反馈信号的俯仰姿态稳定系统
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摘要
An aircraft pitch attitude stabilization system that utilizes an engine pressure ratio signal to cancel pitching moments due to changes in engine thrust. The changes in the engine pressure ratio signals which result from thrust changes are used to generate a pitch stabilization signal that is combined with other pitch control signals to automatically counteract pitching moments resulting from the changes in engine thrust.
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