Electrical shock absorber for docking control system
Abstract
Results are reported from a preliminary experimental study examining an electromechanical actuator for a docking system in space, with emphasis on the attenuation and shock-absorbing characteristics of the actuator. A laboratory prototype of an electromechanical docking system which uses a sonar ranging system as a substitute for the laser range sensor and is controlled by a microprocessor is presented. The configuration of the experimental system consists of a rack and pinion gear actuator, a servo motor, sensors, a digital controller and an air-lifted docking target. For the design of the attenuator controller, the linear quadratic Gaussian (LQG) control design method is applied. For the purpose of attenuation on a specified frequency band, the application of a frequency-weighted LQG method and frequency domain method such as H2 and H-infinity control theory are considered.
- Publication:
-
Joint U.S./Japan Conference on Adaptive Structures
- Pub Date:
- 1991
- Bibcode:
- 1991adst.conf..332N
- Keywords:
-
- Electromechanical Devices;
- Optimal Control;
- Orbital Servicing;
- Shock Absorbers;
- Spacecraft Docking;
- Energy Absorption;
- Linear Quadratic Gaussian Control;
- Space Shuttles;
- Space Stations;
- Spacecraft Design, Testing and Performance