| 摘要 |
PURPOSE: A thrust vectoring flight vehicle with an attitude control module is provided for horizontally flying with an erect attitude at a low speed by the posture control module. CONSTITUTION: A thrust vectoring flight vehicle(100) comprises a fuselage(110), a thrust vectoring system(150), a gyro sensor(195), a control module(170), and a attitude control module(290). The thrust vectoring system changes the thrust direction of a jet engine(140) for the fuselage to horizontally fly. The control module is installed inside the fuselage, and electrically connected to the thrust vectoring system and the gyro sensor. The control module operates the thrust vectoring system by receiving information on the attitude of the fuselage from the gyro sensor. The attitude control module comprises a thruster(291), a propelling hole(297), a jetting pipe(293), and an opening and closing control valve(295). The jetting pipe connects the thruster and the propelling hole to jet propellants to the outside. The opening and closing control valve controls the quantity of the propellants.
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