GUIDANCE SYSTEM FOR FLYING OBJECT AND FLYING OBJECT HAVING THE SAME

摘要

The present invention provides a flying object posture control apparatus, comprising: a turbine unit having an inlet through which a fluid is introduced to an inner space; a lateral force generation unit coupled to the turbine unit so as to have the inner space, and discharging the fluid introduced to the inner space, to a flow path formed on at least one region of an outer circumference thereof to generate a lateral force; and a roll control unit for controlling a discharge direction of the fluid by using a relative rotary motion of the turbine unit, and between the lateral force generation unit and the flying object body so as to control a flying direction of the flying object body coupled to the turbine unit and the lateral force generation unit to be able to rotate.