|発明の名称||FLIGHT VEHICLE AND CONTROL METHOD FOR FLIGHT VEHICLE|
PROBLEM TO BE SOLVED: To provide a flight vehicle which can be accurately and easily moved to a desired position, and a control method for the flight vehicle.
SOLUTION: First, second, third and fourth propellers 40A, 40B, 40C, 40D are so located as to surround a body part 10 on a reference plane rs, and are supported by first, second, third and fourth movable support mechanisms 30A, 30B, 30C, 30D so as to be capable of changing directions of first, second, third and fourth thrusts. When the body part 10 is so flown as to advance in a first direction D1 from an intersection part O towards between the second and third propellers 40B, 40C, the first and second movable support mechanisms 30A, 30B are so controlled that directions of the first and second thrusts are directed to oblique inner, oblique upper and oblique front sides with respect to the first direction D1. The third and fourth movable support mechanisms 30C, 30D are so controlled that directions of the third and fourth thrusts are directed to oblique outer, oblique upper and oblique front sides with respect to the first direction D1.
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