METHOD OF FLIGHT CONTROL FOR ADVANCED GUIDED PARAFOIL AIRBORNE SYSTEM

摘要

A flight control method of a transporting system of a parafoil guide parachute is provided to rapidly and accurately transfer the freight to the destination by measuring the position data and the angle of azimuth in real time and analyzing the effect of the wind. A flight control method of a transporting system of a parafoil guide parachute comprises a step(S10) of inputting the destination; a step(S60) of judging the free flight starting time; a step(S80) of measuring the latitude, the longitude, the height, and the angle of azimuth; a step(S90) of calculating the expected flight path and the expected flight time; a step(S100) of calculating the upper and lower limit flight angles; a step(S110) of analyzing the effect of the wind; a step(S120) of deciding the flight control mode; and a step(S130) of controlling the servo actuator.