HIGH-PERFORMANCE LANDSAT/SPOT DUAL S-/XBAND TELEMETRY TRACKING AND RECEIVING SYSTEM

International Telemetering Conference Proceedings / October 13-16, 1986 / Riviera Hotel, Las Vegas, Nevada === A high-performance dual S/X-band telemetry tracking and receiving system has been developed to provide a low-cost earth station for receiving high-resolution data from current and future LA...

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Main Authors: Bollermann, Bruce, Harshbarger, Roger, Haynie, Mark, Pande, Kailash
Other Authors: SPACE DATA CORPORATION
Language:en_US
Published: International Foundation for Telemetering 1986
Online Access:http://hdl.handle.net/10150/615277
http://arizona.openrepository.com/arizona/handle/10150/615277
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spelling ndltd-arizona.edu-oai-arizona.openrepository.com-10150-6152772016-07-02T03:01:27Z HIGH-PERFORMANCE LANDSAT/SPOT DUAL S-/XBAND TELEMETRY TRACKING AND RECEIVING SYSTEM Bollermann, Bruce Harshbarger, Roger Haynie, Mark Pande, Kailash SPACE DATA CORPORATION International Telemetering Conference Proceedings / October 13-16, 1986 / Riviera Hotel, Las Vegas, Nevada A high-performance dual S/X-band telemetry tracking and receiving system has been developed to provide a low-cost earth station for receiving high-resolution data from current and future LANDSAT/Spot polar orbiting satellites. The antenna system consists of a dual S/X-band telemetry tracking feed in a Cassegrain configuration with a 10-meter parabolic reflector designed for 100 mph wind loading and 10 deg/sec accelerations. The 2 antenna system is mounted to a newly-developed elevation-over-azimuth tracking pedestal, which incorporates the latest technology in a dual brushless d.c. servo motor torque-biased drive train for each axis. This drive train provides an exceptionally wide dynamic range in trlcking velocities for very slow horizon tracking and very fast velocities for near-overhead passes. A microprocessor-based servo control system using the latest state variables feedback and adaptive control techniques is used to provide accurate tracking for both slow and fast rates. A 15-km satellite pass distance from overhead is used as a control system design criterion. For the narrow beamwidth X-band track this requires an acceleration error of less than 0.100 degree and an acceleration error constant of at least 90 sec . The requirement for a high-performance servo system with the low -2 structural resonances of a large antenna constitutes a difficult stability problem. 1986-10 text Proceedings 0884-5123 0074-9079 http://hdl.handle.net/10150/615277 http://arizona.openrepository.com/arizona/handle/10150/615277 International Telemetering Conference Proceedings en_US http://www.telemetry.org/ Copyright © International Foundation for Telemetering International Foundation for Telemetering
collection NDLTD
language en_US
sources NDLTD
description International Telemetering Conference Proceedings / October 13-16, 1986 / Riviera Hotel, Las Vegas, Nevada === A high-performance dual S/X-band telemetry tracking and receiving system has been developed to provide a low-cost earth station for receiving high-resolution data from current and future LANDSAT/Spot polar orbiting satellites. The antenna system consists of a dual S/X-band telemetry tracking feed in a Cassegrain configuration with a 10-meter parabolic reflector designed for 100 mph wind loading and 10 deg/sec accelerations. The 2 antenna system is mounted to a newly-developed elevation-over-azimuth tracking pedestal, which incorporates the latest technology in a dual brushless d.c. servo motor torque-biased drive train for each axis. This drive train provides an exceptionally wide dynamic range in trlcking velocities for very slow horizon tracking and very fast velocities for near-overhead passes. A microprocessor-based servo control system using the latest state variables feedback and adaptive control techniques is used to provide accurate tracking for both slow and fast rates. A 15-km satellite pass distance from overhead is used as a control system design criterion. For the narrow beamwidth X-band track this requires an acceleration error of less than 0.100 degree and an acceleration error constant of at least 90 sec . The requirement for a high-performance servo system with the low -2 structural resonances of a large antenna constitutes a difficult stability problem.
author2 SPACE DATA CORPORATION
author_facet SPACE DATA CORPORATION
Bollermann, Bruce
Harshbarger, Roger
Haynie, Mark
Pande, Kailash
author Bollermann, Bruce
Harshbarger, Roger
Haynie, Mark
Pande, Kailash
spellingShingle Bollermann, Bruce
Harshbarger, Roger
Haynie, Mark
Pande, Kailash
HIGH-PERFORMANCE LANDSAT/SPOT DUAL S-/XBAND TELEMETRY TRACKING AND RECEIVING SYSTEM
author_sort Bollermann, Bruce
title HIGH-PERFORMANCE LANDSAT/SPOT DUAL S-/XBAND TELEMETRY TRACKING AND RECEIVING SYSTEM
title_short HIGH-PERFORMANCE LANDSAT/SPOT DUAL S-/XBAND TELEMETRY TRACKING AND RECEIVING SYSTEM
title_full HIGH-PERFORMANCE LANDSAT/SPOT DUAL S-/XBAND TELEMETRY TRACKING AND RECEIVING SYSTEM
title_fullStr HIGH-PERFORMANCE LANDSAT/SPOT DUAL S-/XBAND TELEMETRY TRACKING AND RECEIVING SYSTEM
title_full_unstemmed HIGH-PERFORMANCE LANDSAT/SPOT DUAL S-/XBAND TELEMETRY TRACKING AND RECEIVING SYSTEM
title_sort high-performance landsat/spot dual s-/xband telemetry tracking and receiving system
publisher International Foundation for Telemetering
publishDate 1986
url http://hdl.handle.net/10150/615277
http://arizona.openrepository.com/arizona/handle/10150/615277
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