Time-attitude based method for decomposition and synthesis of imaging satellite observation task
An imaging satellite and task decomposition technology, applied in the direction of integrated navigator, etc., can solve the problem of no concept of time, only consider the space position, etc., and achieve the effect of intuitive and efficient target decomposition and synthesis
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[0045] The present invention will be further described below by specific examples.
[0046] Time-attitude vector of 1-point target
[0047] The latitude and longitude heights of the point target (Target) in the WGS84 coordinate system are b, l, and h respectively, and the position of the satellite at time t in the J2000 geocentric inertial coordinate system is The pointing attitude of the satellite to the target at time t in the orbital coordinate system is When calculating the positional relationship between the satellite and the target, they can be transformed into a coordinate system.
[0048] For a satellite flying normally, the position of the satellite is a function of time, and the position of the satellite at a certain time in the future can be predicted by using the high-precision ephemeris prediction method, that is, the position of the satellite corresponds to the time point one by one:
[0049]
[0050] The position of the target can be converted to the posi...
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