Parallel-filter observer control with CCD measurements for space optical communication equipment on a moving platform
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Summary
This summary is machine-generated.This study introduces a parallel-filter observer to stabilize line-of-sight (LOS) for space optical communication, overcoming bandwidth limits for trajectory tracking with charge-coupled device (CCD) measurements.
Area Of Science
- Aerospace Engineering
- Optical Communication Systems
- Control Systems Theory
Background
- Space optical communication missions require precise line-of-sight (LOS) stabilization for effective trajectory tracking.
- Existing methods face bandwidth limitations with charge-coupled device (CCD) measurements on moving platforms.
- Degradation in stability can occur with single high-bandwidth filters in tracking systems.
Purpose Of The Study
- To develop a novel parallel-filter observer methodology for stabilizing LOS in space optical communication.
- To overcome the bandwidth limitations inherent in current trajectory tracking systems.
- To enhance the stability and tracking performance of gimbals in dynamic space environments.
Main Methods
- Implementation of a parallel-filter observer to stabilize LOS.
- Introduction of an equivalent high-order parallel-filter compensator to reduce controller output.
- Utilization of tracking errors directly for LOS stabilization, avoiding complex target dynamics modeling.
Main Results
- The parallel-filter observer effectively mitigates stability degradation compared to single high-bandwidth filters.
- A stabilized high-bandwidth observer is achieved, enhancing tracking accuracy.
- Simulation and experimental results confirm improved LOS stabilization under carrier disturbance and target motion.
Conclusions
- The proposed parallel-filter observer methodology offers a simple and applicable solution for LOS stabilization in space optical communication.
- It provides excellent tracking performance for engineering applications with limited measurement bandwidth.
- The approach enhances gimbal stability in inertial space and is robust to disturbances.

