The present application relates to a strong static unstable
launch vehicle adaptive and robust stability control method, gap measurement is performed on the rated and deviation models and the nominal model at different times of the whole flight segment, the segmentation of the rated and deviation models in the time dimension is completed, and the robust controller in each segment is designed; the nominal model is tuned by using
loop shaping method to obtain the model G s ; the model G s is obtained by
order reduction of G sb , the uncertainty envelope between G sb and the rated and deviation
model set is measured to obtain the controlled object G p containing multiplicative uncertainty; the control weight function W u and the error weight function W e are designed; G p , W u and W e are formed into a generalized
robust control design object P, which is substituted into the
robust control design architecture, and the robust controller is obtained by using the mu synthesis
iterative method and
order reduction; the adaptive adjustment law of the
loop gain is designed and multiplied by the robust controller to stabilize the flight attitude of the
launch vehicle in the current segment. The problem of
attitude stability control of a strong static unstable
launch vehicle is solved.