A digital computer-based state variable controller was designed and applied to the 70-m antenna axis servos. The general equations and structure of the algorithm and provisions for alternate position error feedback modes to accommodate intertarget slew, encoder referenced tracking, and precision tracking modes are descibed. Development of the discrete time domain control model and computation of estimator and control gain parameters based on closed loop pole placement criteria are discussed. The new algorithm was successfully implemented and tested in the 70-m antenna at Deep Space Network station 63 in Spain
The design of a new position loop controller for the 34-meter High Efficiency Deep Space antennas us...
This paper discusses the compensation of antenna-pointing errors following the recent analysis and r...
The feasibility of using inertial instruments to determine the pointing attitude of the NASA Deep Sp...
A control axis referenced model of the NASA/JPL 70-m antenna structure is combined with the dynamic ...
The design of control mode switching algorithms and logic for JPL's 70 m antenna servo controller ar...
A modified output prediction procedure and a new controller design is presented based on the predict...
Dynamic models for the various functional elements of the 70 m antenna axis servos are described. Th...
The objective of this study is to investigate the feasibility of a pointing (position loop) controll...
The application of small computers using digital techniques for operating the servo and control syst...
The elevation and azimuth servo rate loops at the 34-m High Efficiency Deep Space Station 15 (DSS 15...
A digital computer program was generated which mathematically describes an optimal estimator-control...
International Telemetering Conference Proceedings / October 30-November 02, 1989 / Town & Country Ho...
An improvement of pointing precision of the DSS-14 antenna is planned for the near future. In order ...
This work is the first step toward increasing the bandwidth of the DSS-13 antenna position loop cont...
Analytic methods for evaluating pointing errors caused by external disturbance torques are developed...
The design of a new position loop controller for the 34-meter High Efficiency Deep Space antennas us...
This paper discusses the compensation of antenna-pointing errors following the recent analysis and r...
The feasibility of using inertial instruments to determine the pointing attitude of the NASA Deep Sp...
A control axis referenced model of the NASA/JPL 70-m antenna structure is combined with the dynamic ...
The design of control mode switching algorithms and logic for JPL's 70 m antenna servo controller ar...
A modified output prediction procedure and a new controller design is presented based on the predict...
Dynamic models for the various functional elements of the 70 m antenna axis servos are described. Th...
The objective of this study is to investigate the feasibility of a pointing (position loop) controll...
The application of small computers using digital techniques for operating the servo and control syst...
The elevation and azimuth servo rate loops at the 34-m High Efficiency Deep Space Station 15 (DSS 15...
A digital computer program was generated which mathematically describes an optimal estimator-control...
International Telemetering Conference Proceedings / October 30-November 02, 1989 / Town & Country Ho...
An improvement of pointing precision of the DSS-14 antenna is planned for the near future. In order ...
This work is the first step toward increasing the bandwidth of the DSS-13 antenna position loop cont...
Analytic methods for evaluating pointing errors caused by external disturbance torques are developed...
The design of a new position loop controller for the 34-meter High Efficiency Deep Space antennas us...
This paper discusses the compensation of antenna-pointing errors following the recent analysis and r...
The feasibility of using inertial instruments to determine the pointing attitude of the NASA Deep Sp...