The invention relates to a
frequency management method for stable postures of a hypersonic aircraft. The method sequentially comprises the steps that (1), information of various frequencies is collected; (2) when a
rigid motion transmission band is larger than first-order
elastic vibration frequency by more than 10 times, and an elasticity amplitude stabilizing method is adopted; (3), a rate
gyroscope is led in to a place where the vibration mode slope is zero; (4) when shaking
zero frequency is larger than
pole frequency, shaking stability is improved through feedback of an
accelerometer or additional arrangement of an anti-shaking board; (5), a transmission band of a steering engine is 5-10 times of the
rigid motion transmission band; (6), an
inertia unit transmission band is 10-20 times of
rigid motion bandwidth; (7), the structural stiffness of an executing mechanism and a sensitive mechanism is kept to be more than 5 times of a single-engine bandwidth; (8), main frequency of external disturbance is prevented from being coupled with inherent frequency of a structural part; (9), ground tests of various frequency characteristics are carried out, and the stable postures of the hypersonic aircraft are ensured. According to the
frequency management method for the stable postures of the hypersonic aircraft, repeated schemes are avoided, development schedule is accelerated, and
system interfaces are made to be clear and comprehensively optimum.