Aircraft air refueling mode control method

• Main Authors: XIANG MEI, ZHANG YUBAI, LENG GUOQI, XIE HUICI, YU YUNPENG, HUANG YONGQIANG, WENG XUEHUA, ZHANG KUN
• Format: Patent
• Language: Chinese; English
• Published: 28.05.2024
• Subjects: CONTROLLING; PHYSICS; REGULATING; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES

The invention relates to an aircraft air oil receiving mode control method, which comprises the following steps of: reasonably voting atmosphere and attack angle measurement signals of a flight control system in an air oil receiving process, and simultaneously processing a control law algorithm, so that the air oil receiving mode of an aircraft can be controlled. According to the invention, under the condition that the air and attack angle measurement signals of the oil receiver aircraft are influenced by the interference airflow of the oiling machine, the dynamic and static pressure and attack angle measurement signals of the control law of the flight control system of the oil receiver aircraft are automatically processed, so that the influence of the interference airflow of the oiling machine on the oil receiver aircraft is avoided, and the flight safety of the aircraft is guaranteed. 一种飞机空中受油模态控制方法，在空中受油过程中对飞行控制系统的大气和迎角测量信号进行合理表决，同时对控制律算法进行处理，即能控制飞机空中受油模态。本发明能够在受油机大气和迎角测量信号受到加油机干扰气流影响的情况下，自动对受油机飞行控制系统控制律的动