Exact(20)
The use of Pontryagin's maximum principle to solve spacecraft motion control problems is demonstrated.
Similarly, the spacecraft motion, which has positive velocity away from the Earth, causes a positive shift in the counter.
Finally we calculate the energy shift due to the spacecraft motion for each individual looking direction of the instrument.
In addition different optical arrangements have been analysed and their effects on the cancellation of the spacecraft motion is discussed.
This no longer allows the spacecraft motion to be synchronized to the super-rotating atmosphere and affects the longitudinal coverage and the spatial resolution of images.
Restoration is further complicated by incomplete knowledge of the PSF and the time variance resulting from changes in focus and spacecraft motion.
Similar(40)
The dashed arrows indicate the direction of spacecraft spin motion.
Therefore, a large variation in photoelectron flux associated with the spacecraft spin motion is not expected.
Due to the spacecraft spin motion, the fan-shaped FOV scans the entire sky once a spin.
A simple model of the spacecraft relative motion is used in MPC to decrease the computational burden.
The aperture of 360° near the sensor top provides a 4 − π sr field-of-view (FOV) by using the spacecraft spin motion.
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