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Radeus Labs
Radeus Labs - Series 9000 Antenna Control System (ACS)
Condition:
New
Weight:
226.80 KGS
Width:
121.92
(cm)
Height:
152.40
(cm)
Depth:
40.64
(cm)
Request a quote at Contact@orbitalconnect.com or +1.888.315.9545
Radeus Labs - Series 9000 Antenna Control System (ACS)
Dependable, high-precision tracking High-performance antenna control system focusing on multi-motor-per-axis, full-motion antenna solutions. Supports monopulse tracking with a variety of feed configurations.
Features
- Touchscreen controls
- Efficient, intuitive GUI
- Up to four Antenna Control Panels (ACP)
- Setup Wizard for easy configuration
- Ethernet SNMP or REST API remote interfaces
- Single, dual-, and multi-motor configurations per axis
- Up to 16 E-Stops
- Final, Pre and Velocity limit inputs
- Stow-pin interlocks and actuation
- Auxiliary drive integration
- Torque biasing of multi-motor applications
- Support for synchronous AC, asynchronous AC, and brushless DC motor opitons
Options
- Monopulse tracking option
- Rack or cabinet drive enclosures
- L, C, S, Ku band beacon receivers available
- CP/LP switching control
Pointing & Tracking
- Position control to within 0.0005 degrees RMS error
- Steptrack accuracy to within 10% RMS of -3dB beamwidth
- Predictive Track accuracy to within 5% RMS of -3dB beamwidth
- Monopulse tracking to within 3% RMS of -3dB beamwidth
| Models |
Model 9000 Tracking Receiver, Model 9050 Drive Cabinet |
|---|---|
| Steptrack |
Tracking algorithm performing periodic and or level triggered scans to peak up signal strength (requires beacon receiver). |
| Predictive Track |
Points the satellite dish using an orbital model created from previous AZ and EL step-track data (requires beacon receiver). |
| Monopulse |
Automatically acquires target, peak phase align and calibrate to begin tracking with monopulse tracking receiver. Transfers to predictive model or ephemeris tracking on loss of monopulse signal. |
| NORAD TLE |
Automated tracking based on NORAD two-line element sets |
| Intelsat (IESS-412) |
Tracking derived from Intelsat 11-element parameter sets |
| TLE with Steptrack |
Track using TLE as a base model but add periodic Step Tracks to correct for offsets over time |
| IESS-412 with Steptrack |
Tracking with Intelsat model, with added Step Track to correct for offsets over time |
| Manual Jog |
Dedicated front-panel antenna jog controls |
| Move to Longitude |
Points the antenna to AZ and EL angles determined by the longitudinal orbital slot |
| Move to Look Angles |
Points the antenna to user-supplied AZ, EL and POL angles |
Performance – Flexible tracking modes, intuitive menu layouts and a compact parameter set keep your antenna applications on point.
Availability – We understand the need for quick delivery. Lean manufacturing methods allow us to ship most systems within 30 days of an accepted order!
World-Class Support – You are never on your own with a Radeus Labs product. The experts at Radeus Labs are standing by if you need help.
The 9000 ACS provides a flexible solution for multi-motor per axis and monopulse tracking applications. It is adaptable to multiple antenna makes for retrofits and works equally well on new antennas. The Setup Wizard, flexible position feedback options, and
diagnostic logs are just a few of the features that make the 9000 ACS the best solution for your full motion antenna systems.
Modes of Operation
Manual — Front-panel buttons for two-speed, manual jog control.
Move to Longitude — Position to AZ and EL angles determined from the longitudinal orbital slot.
Move to Look Angles — Position to user-provided AZ, EL, and POL angles.
Step Track — Periodic algorithm to perform an AZ-EL scan pattern to peak up signal strength.
Predictive Track — Point the satellite dish using an orbital model created from previous peak AZ and EL step-track data points.
TLE (Two-Line Element) — Track automated positioning based on NORAD two-line element sets.
TLE with Steptrack — Steptrack incorporated with TLE to provide closed loop correction and superior pointing accuracy.
Intelsat-11 — Automated tracking to AZ and EL coordinate sets derived from Intelsat 11 parameters.
Intelsat-11 with Steptrack — Steptrack incorporated with Intelsat-11 to provide closed loop correction and superior pointing accuracy.
Computer Track — Automated positioning using commanded angles supplied from an external computer.
Sun and Moon Track — Automated positioning to AZ and EL locations of the sun and the moon.
Star Track — Automated positioning to AZ and EL locations of radio stars.
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Details
Radeus Labs - Series 9000 Antenna Control System (ACS)
Dependable, high-precision tracking High-performance antenna control system focusing on multi-motor-per-axis, full-motion antenna solutions. Supports monopulse tracking with a variety of feed configurations.
Features
- Touchscreen controls
- Efficient, intuitive GUI
- Up to four Antenna Control Panels (ACP)
- Setup Wizard for easy configuration
- Ethernet SNMP or REST API remote interfaces
- Single, dual-, and multi-motor configurations per axis
- Up to 16 E-Stops
- Final, Pre and Velocity limit inputs
- Stow-pin interlocks and actuation
- Auxiliary drive integration
- Torque biasing of multi-motor applications
- Support for synchronous AC, asynchronous AC, and brushless DC motor opitons
Options
- Monopulse tracking option
- Rack or cabinet drive enclosures
- L, C, S, Ku band beacon receivers available
- CP/LP switching control
Pointing & Tracking
- Position control to within 0.0005 degrees RMS error
- Steptrack accuracy to within 10% RMS of -3dB beamwidth
- Predictive Track accuracy to within 5% RMS of -3dB beamwidth
- Monopulse tracking to within 3% RMS of -3dB beamwidth
| Models |
Model 9000 Tracking Receiver, Model 9050 Drive Cabinet |
|---|---|
| Steptrack |
Tracking algorithm performing periodic and or level triggered scans to peak up signal strength (requires beacon receiver). |
| Predictive Track |
Points the satellite dish using an orbital model created from previous AZ and EL step-track data (requires beacon receiver). |
| Monopulse |
Automatically acquires target, peak phase align and calibrate to begin tracking with monopulse tracking receiver. Transfers to predictive model or ephemeris tracking on loss of monopulse signal. |
| NORAD TLE |
Automated tracking based on NORAD two-line element sets |
| Intelsat (IESS-412) |
Tracking derived from Intelsat 11-element parameter sets |
| TLE with Steptrack |
Track using TLE as a base model but add periodic Step Tracks to correct for offsets over time |
| IESS-412 with Steptrack |
Tracking with Intelsat model, with added Step Track to correct for offsets over time |
| Manual Jog |
Dedicated front-panel antenna jog controls |
| Move to Longitude |
Points the antenna to AZ and EL angles determined by the longitudinal orbital slot |
| Move to Look Angles |
Points the antenna to user-supplied AZ, EL and POL angles |
Performance – Flexible tracking modes, intuitive menu layouts and a compact parameter set keep your antenna applications on point.
Availability – We understand the need for quick delivery. Lean manufacturing methods allow us to ship most systems within 30 days of an accepted order!
World-Class Support – You are never on your own with a Radeus Labs product. The experts at Radeus Labs are standing by if you need help.
The 9000 ACS provides a flexible solution for multi-motor per axis and monopulse tracking applications. It is adaptable to multiple antenna makes for retrofits and works equally well on new antennas. The Setup Wizard, flexible position feedback options, and
diagnostic logs are just a few of the features that make the 9000 ACS the best solution for your full motion antenna systems.
Modes of Operation
Manual — Front-panel buttons for two-speed, manual jog control.
Move to Longitude — Position to AZ and EL angles determined from the longitudinal orbital slot.
Move to Look Angles — Position to user-provided AZ, EL, and POL angles.
Step Track — Periodic algorithm to perform an AZ-EL scan pattern to peak up signal strength.
Predictive Track — Point the satellite dish using an orbital model created from previous peak AZ and EL step-track data points.
TLE (Two-Line Element) — Track automated positioning based on NORAD two-line element sets.
TLE with Steptrack — Steptrack incorporated with TLE to provide closed loop correction and superior pointing accuracy.
Intelsat-11 — Automated tracking to AZ and EL coordinate sets derived from Intelsat 11 parameters.
Intelsat-11 with Steptrack — Steptrack incorporated with Intelsat-11 to provide closed loop correction and superior pointing accuracy.
Computer Track — Automated positioning using commanded angles supplied from an external computer.
Sun and Moon Track — Automated positioning to AZ and EL locations of the sun and the moon.
Star Track — Automated positioning to AZ and EL locations of radio stars.
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