ObservedParameters.calculate_observation_jacobian

ObservedParameters.calculate_observation_jacobian

ObservedParameters.calculate_observation_jacobian(txrx_pass, space_object, variables, deltas, transforms={}, **kwargs)

Calculate the observation and its Jacobean of a pass of a specific space object given the current state of the Scheduler.

The Jacobean assumes that the SpaceObject has a Orbit state. To perturb non Orbit states a custom implementation is needed.

NOTE: During the numerical calculation of the Jacobean only the range and range rates are calculated and calculate_snr=False.

#TODO: Docstring