The invention discloses a closed-
loop control method for controlling the output
energy margin of a solar array, which relates to the field of
autonomous management of on-
orbit energy of a
satellite power supply subsystem. The method comprises the following steps: 1, a
satellite coordinate
system OXYZ is established; 2, a solar array on the
satellite is set to track rotation of the run at an
angular velocity omega0 around the Y axis; 3, the lagging angle of the initial solar array is set to be alpha; 4, the output power psa of the solar array in a solar
irradiation area at a previous moment iscalculated; 5, the
energy margin Wsp of the solar array in an
orbit circle is calculated; 6, the Wsp is judged respectively, and whether the solar array
energy margin Wsp is in an energy excessive state or a serious power shortage state or an insufficient output energy state is judged; and 7, the solar array is adjusted to realize closed-
loop control on the output energy margin of the solar array.
Rotation control of the solar array is incorporated into the allocation process of the satellite
energy system, and control on the output energy margin of the solar array is realized.