LinkAlign-360MPT-41 — Auto Acquisition and Program Tracking Positioner

Overview

The LinkAlign-360MPT-41 is an auto-acquisition azimuth and elevation positioner designed for satellite communications. It features an embedded controller with a built-in GPS and digital compass to automatically point directional antennas.

Technical Summary

This positioner incorporates a full-featured web-based user interface for manual control, status monitoring, and a stored satellite database. It utilizes two-line element set program tracking to follow low and medium earth orbit (LEO/MEO) satellites.

Operational Use Cases

The system is used for establishing and maintaining satellite communications, specifically targeting LEO and MEO constellations. It supports automated pointing for secure data links and tactical communication networks.

Deployment Environments

This positioner supports fixed-site installations and transportable tactical platforms that require automated satellite tracking and reliable directional communications.

Performance Metrics

• Payload Capacity: Up to 160 lbs (72.6 kg) with included counterweights
• Azimuth Range: 480° (±240°)
• Elevation Range: 190°, configurable to (+180°/-5°) or (+95°/-95°)

Setup & Portability

The positioner operates via Power over Ethernet (PoE) for streamlined cabling and power delivery. It includes counterweights for payload balancing and features a web-based user interface for rapid pointing configuration.

Compatibility

The unit is typically paired with 3-foot to 6-foot antennas. It features a command line interface for direct integration into larger system architectures and controllers.

FAQs

• Why use an automated positioner with a directional antenna? Directional antennas provide more secure communications than omnidirectional options by concentrating the signal and reducing interception risk. Automated positioners provide the continuous, accurate pointing required to maintain these directional links.
• What is two-line element set program tracking? Two-line element (TLE) data provides the orbital parameters needed to predict a satellite's path. Positioners use this data to automatically calculate and follow the trajectories of low and medium earth orbit satellites.
• What payload specifications must be verified prior to installation? Confirm the total weight of the antenna and mounting hardware does not exceed the positioner's maximum payload capacity. Verify the attachment method and physical dimensions against the manufacturer's mechanical drawings.
• Problems we solve: where do we start with incomplete requirements? An incomplete specification can make product selection difficult. Start by sharing the task, operating environment and known constraints with Cyntony so the team can help define what to verify and which options are worth discussing (Our process).
• Outcomes we deliver: what comes from working through the requirements? The practical outcome is a requirements-led set of product options to evaluate with Cyntony. Confirm performance, compatibility and any service scope for your configuration before selection (Our process).

Video Notes

Consider a video demonstrating the web-based user interface, the command line integration process, and a time-lapse of the positioner executing a programmed LEO/MEO tracking maneuver.