The application discloses a design method of a net-catch load effective capture
caliber, which comprises the following steps: acquiring multi-directional contour size parameters of a waste
satellite; generating a position aiming parameter of an aircraft relative to the waste
satellite when launching the net-catch load based on the multi-directional contour size parameters; acquiring an installation position parameter of the net-catch load relative to the
mass center of the aircraft; estimating a capture
flight time t net and a deployment efficiency η of the net-catch load; and calculating an effective capture
caliber R of the net-catch load based on the multi-directional contour size parameters of the waste
satellite, the position aiming parameter of the aircraft relative to the waste satellite when launching the net-catch load, the installation position parameter, the capture
flight time and the deployment efficiency. net The effective capture
caliber of the net-catch load can be designed according to the contour size of the waste satellite, the position aiming parameter of launching, the installation position of the load, the capture
flight time and the deployment efficiency, and reliable capture of waste satellites with different contour features is realized.