Article Active disturbance rejection control of drag-free satellites considering the effect of micro-propulsion noise

The space gravitational wave detection mission requires a super "static and pre-cise" scientific experiment environment. In order to solve the non-conservative force disturbance variation and the actuator noise and measurement noise, this paper designs a drag-free control scheme based on active disturbance rejection control (ADRC) framework to achieve the high-precision index. According to the ultra-high accuracy, low bandwidth limitation, and robustness requirements of drag-free satellite, the HN controller satisfying the robustness constraint is de-signed as an active disturbance rejection feedback controller to achieve the high -precision index. Meanwhile, the non-conservative force disturbance with a wide range of variations is estimated and feedforward compensated by an extended state observer to improve the system robustness. Simulation results show that the control system can achieve the relative displacement of 2 nm/Hznm/Hz(1/2) for the drag-free satellite platform and the residual acceleration of 1 3 10(-15) m/sm/s(2)/Hz(1/2) for the test mass.