Single-ring patrol configuration design method for high-orbit satellite area protection

The invention discloses a single-ring patrol configuration design method for high-orbit satellite area protection. The method comprises the following steps: inputting the number of protection objects, the orbit distribution position, the protection distance and the number of patrol satellites in the high-orbit satellite area protection; determining a radius range and a phase range of a protection area orbit according to the guard distance, the orbit distribution position and the number of the protection objects, and then calculating the transfer time and the speed increment of west descending and east ascending of the patrol satellite; calculating the transfer time of the east floating and west floating processes of the patrol satellite; calculating the inspection cycle of the high-orbit satellite area protection single-ring inspection configuration, calculating the fuel consumption of each inspection satellite in the high-orbit satellite area protection single-ring inspection configuration, and completing th