This application discloses a method and apparatus for cooperative containment guidance of aircraft, relating to the field of aircraft guidance and control. The method includes acquiring the position, velocity, heading angle, interception time, navigation ratio of the pursuing aircraft, position, velocity, heading angle of the defending aircraft, target position, and target heading angle of the pursuing aircraft; determining the coordinates of the containment point using a
geometric programming method; and controlling the target and the defending aircraft using a cooperative guidance method based on the coordinates of the containment point, the navigation ratio of the pursuing aircraft, the position, velocity, heading angle of the pursuing aircraft, the position, velocity, heading angle of the defending aircraft, the target position, and the target heading angle of the defending aircraft, thereby achieving cooperative containment of the pursuing aircraft. This application improves the effectiveness of the cooperative containment guidance strategy and the interception efficiency of the pursuing aircraft.