ROCKET GUIDANCE COMPUTING DEVICE, ROCKET GUIDANCE SYSTEM, ROCKET, ROCKET GUIDANCE COMPUTING PROGRAM, AND ROCKET GUIDANCE COMPUTING METHOD OF ROCKET GUIDING COMPUTING DEVICE

摘要

PROBLEM TO BE SOLVED: To guide a solid rocket without a thrust cutoff function with high accuracy.

SOLUTION: A prediction state quantity computing part 120 computes a prediction state quantity 193 of the rocket based on a speed vector V, a position vector R and a prediction profile 191. A request state quantity computing part 130 computes a request state quantity 194 of the rocket based on target orbital information 192 and the prediction profile 191. A thrust direction determination part 140 computes the update amount of steering coefficient based on a state quantity error of the prediction state quantity 193 and the request state quantity 194. A thrust direction determination part 140 updates the steering coefficient based on the update amount of the steering coefficient.

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