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Algorithms for command control of hypersonic aircraft at the climbing leg

Victor Balakin
The problem of forming sampling control with forecast (command control) for a hypersonic cruising aircraft at the climbing leg is considered. The motion is analyzed under the atmospheric density disturbance and deviations from aerodynamic characteristics of the aircraft. Two control algorithms are suggested: one-channel (by the angle of attack) and two-channel (by the angle of attack and fuel consumption per second).
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