Patch Effect in Drag-Free Satellites

To compensate for the non–gravitational orbital disturbances drag free satellites monitor and control their position with respect to a reference body enclosed inside their structure. The body, shielded from the environment, follows a free fall trajectory when its motion can be ideally considered decoupled from that of the spacecraft. Lessons learned from Gravity Probe B and the design of the Satellite Test of the Equivalence Principle experiment strongly motivate the study of the force and torque between the reference body and the spacecraft due to uneven distributions of electrostatic potentials. Additional interest to that comes also from prospective space experiments as Microscope and the Laser Interferometer Space Antenna.