SimulateStarCameraTerrasar

This program simulates outputfileStarCamera measurements at each satellite's position for the Terrasar satellite. The inputfileOrbit must contain positions and velocities (see OrbitAddVelocityAndAcceleration). The resulting rotation matrices rotate from satellite frame to inertial frame.

H. Fiedler, E. Boerner, J. Mittermayer and G. Krieger, Total zero Doppler Steering-a new method for minimizing the Doppler centroid, in IEEE Geoscience and Remote Sensing Letters, vol. 2, no. 2, pp. 141-145, April 2005, https://www.doi.org/10.1109/LGRS.2005.844591.

Name	Type	Annotation
outputfileStarCamera	filename	rotation from satellite to inertial frame (x: along, y: cross, z: nadir)
inputfileOrbit	filename	position and velocity defines the orientation of the satellite at each epoch

This program is parallelized.