Fuselage return control method and system for simulating flight of unmanned aerial vehicle

• Main Authors: WANG ZHENG, GUO JIANJUN, LI SHILIN, XI QIANWEN
• Format: Patent
• Language: Chinese; English
• Published: 07.03.2023
• Subjects: AMUSEMENTS; CARD, BOARD, OR ROULETTE GAMES; GAMES; GAMES NOT OTHERWISE PROVIDED FOR; HUMAN NECESSITIES; INDOOR GAMES USING SMALL MOVING PLAYING BODIES; SPORTS; VIDEO GAMES

The invention provides a fuselage return control method for simulating flight of an unmanned aerial vehicle. The fuselage return control method comprises the following steps: recording a simulated unmanned aerial vehicle movement input value; respectively setting the input value to a forward movement value and a rightward movement value, and calculating a first product of the forward movement value and a forward movement vector and a second product of the rightward movement value and a rightward movement vector; judging whether the unmanned aerial vehicle is static or not according to the sum of absolute values of the first product and the second product, and if not, calling a floating point value WingAngle and an input value or a reverse input value; and determining the rotation value of the simulated unmanned aerial vehicle according to the WingAngle, determining the angle value of the unmanned aerial vehicle according to the input value or the reverse input value, and executing return control based on the