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Overview: The optical-electric tracking system characterizes a high-dynamic tracking system with the only line of sight error available, and its tracking accuracy is one of the key indexes for the optical–electric tracking control system. Precision control methodologies are necessary tools to implement high-precision tracking performance. Facing different applying areas, the tracking control system has to have a different performance to satisfy with conditions, and need to require high-performance control techniques. In another way, control techniques promote the development of the tracking control system. In essence, control methodologies only push the closed-loop performance to close to sensor resolution. Obviously, there is no method to reach this point. So, it is necessary to investigate suitable control methodologies to improve performance of the tracking control system. The optical-electric tracking system from single stage type to the dual-stage type is inseparable from the progress of actuator, sensor, materials, and mechanical structures. But, due to complex disturbances and maneuver target inducing dynamic lag errors in the hash working condition, the tracking performance could not meet the mission. High control bandwidth is usually restricted in a finite sampling rate of a charge-coupled device (CCD) based tracking loop, which hinders a good closed-loop performance. As far as tracking control is concerned, a rate feedforward controller is usually used to improve the control performance; however, it is restricted by the line-of-sight (LOS) rate, which is required to be estimated due to only the LOS error available in the CCD-based tracking control system. Besides that, it is also affected by the inverse of the control model. Vibration rejection is a key technology of practical engineering, especially in optical telescopes with a stable accuracy of μrad level. The closed-loop performance of optical telescopes is largely determined by the control bandwidth, while it is severely limited by the low sampling rate and large time delay of the image sensor, so it is difficult to mitigate structural vibrations in optical telescopes, especially wideband vibrations because they exist universally and greatly affect the stability of the system. Different from general motion control and visual servoing system, the tracking system has to accommodate for being applied in different platforms, which requires solving the three problems of disturbance rejection, target tracking and cooperative position. This paper reviews and investigates state of art control techniques and methodologies in the tracking control system, and also looks into the future research.
Control structure based on acceleration feedback
Acceleration open-loop response
Velocity closed-loop response
Velocity tracking error
Triple-loop control system based on a virtual velocity[71]
Schematic diagram of estimation of initial velocity and position
Schematic diagram of acceleration disturbance[75]
Comparisons of disturbance rejection
1.2 m MoZi communication telescope[76]
The tracking accuracy of 1.2 m telescope in the condition of wind disturbance
Equipment of dual-motor tracking control system
Open-loop velocity Bode response
Tracking error of single and dual motor sinusoidal trajectory
Linear trajectory tracking based on acceleration feedback
Schematic diagram of a gear-box control
Inertial equipment of multiaxis gimbals
Inertial equipment of periscopic sight
Inertial stabilization tip-tilt mirror[35]
Feedforward control of tip-tilt mirror[41]
Schematic diagram of dual-stage platform[89]
Dual-stage stabilization platform in experiments
Frequency response of active disturbance rejection
Tracking control system based on Stewart platform[104]
A tracking control system of a link-parallel mechanism[105]
Predictive control based on a standard Smith method[115-117]
Predictive control based on an improve Smith method[118]
Fractional controller of compensating time delay[119]
Feedforward control method based oncomposite of position encoder
Equivalent feedforward control based on fusion of a gyro[122]
Equivalent feedforward control based on an error observer[50, 59, 51, 123-124]
Azimuth curves of tracking error
Elevation curves of tracking error
Bode response of error attenuation
Tracking error curves
Bode response of Q-filter
Spectra of closed-loop errors with different controllers
Schematic diagram ofdual-stage tracking system
Structure of standard dual-stage control
Unload structure of dual-stage control
Schematic diagram of triple-stage tracking system[25]
Picture of triple-stage control (except gimbal)[30]
Development hierarchy of optical-electric tracking control system