A direct solution method of unbiased current attitude during satellite maneuvering imaging
A mobile imaging and satellite technology, applied in the interpretation of photos, camera devices, etc., can solve the problems of drastic changes in angular velocity and large amount of computation, and achieve the effect of reducing the amount of computation and avoiding iterative calculation of drift angle
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[0062] based on the following Figure 1 ~ Figure 4 , specifically explain the preferred embodiment of the present invention.
[0063] Such as figure 1 As shown, the present invention provides a method for directly solving the non-bias attitude in the process of satellite maneuvering imaging, comprising the following steps:
[0064] Step S1. Calculate the component of the optical axis vector of the spaceborne camera in the orbital coordinate system according to the mission plan and its derivative in the orbital coordinate system
[0065] Step S2. Calculate the expected Euler angle of the spaceborne camera coordinate system relative to the orbital coordinate system rolling axis according to the optical axis vector constraint and the pitch axis expected Euler angle θ, and further calculate the derivative of the expected Euler angle and
[0066] Step S3, according to the constraint that the direction of the image movement velocity must be consistent with the direction ...
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