Smooth and steady pointing maneuvering control method for satellite optical load
A pointing mechanism and optical technology, applied in the field of communication, can solve the problems of fast pointing maneuver control of difficult loads, affecting the pointing stability of the load optical axis, slow attitude maneuvering speed, etc., achieve high target orientation accuracy and stability, and suppress the optical axis Jitter, pointing to the effect of little jitter
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[0030] Specific embodiments of the present invention will be described in detail below.
[0031] Such as figure 1 As shown, a steady pointing maneuver control method for a satellite optical load includes the following steps:
[0032] (1) Stabilize the attitude of the satellite body;
[0033] (2) Control the pointing mechanism of the optical load, so that the pointing mechanism can maneuver to the target position according to the established trajectory;
[0034] (3) Control the image stabilization mechanism to compensate the optical axis shake, and stabilize the image of the target azimuth.
[0035] Further, in step (1), the attitude of the satellite body is stabilized by proportional-derivative control.
[0036] Further, the optical load described in step (2) includes a pointing mechanism 11, a mirror 13, an image stabilization mechanism 17 and an imaging array 15,
[0037] Reflector 13 is fixedly connected with lens barrel 16 by bolts,
[0038] The imaging array 15 is fi...
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