The invention belongs to the technical field of inertial navigation, and particularly relates to a rotation modulation inertial navigation full-state
simulation method. The method is applied to a rotation modulation
inertial navigation system and comprises the following steps: step 1, generating flight path data in a typical flight environment; 2, determining a transposition strategy of the rotation modulation
inertial navigation system, and reversely calculating an angle increment and a speed increment of a sensitive
system of the rotation modulation
inertial navigation system by combining the flight path data in the step 1; step 3, injecting an inertial device error of the rotation modulation inertial
navigation system into the angle increment and the speed increment obtained in the step 2 to obtain the actually output angle increment and speed increment; step 4, the rotation modulation inertial
navigation system performs inertial calculation by using the actually output angle increment and speed increment obtained in the step 3 to generate navigation trajectory data; and 5, performing consistency comparison
verification on the navigation track data generated in the step 4 and the
flight track data in the step 1, and if the consistency comparison
verification is not passed, returning to the step 2 to update the transposition strategy until the consistency comparison
verification is passed. And the shafting arrangement, the rotation strategy and the
inertia calculation process of the rotation modulation inertial navigation under any aircraft maneuver are comprehensively verified.