LinkAlign-360MPT-40 — Auto Acquisition Satellite Antenna Positioner

Overview

The LinkAlign-360MPT-40 is an auto-acquisition positioner designed to automatically point directional antennas for satellite communications. It features an embedded antenna controller, a built-in GPS, and a digital compass for rapid, accurate alignment without external heading sensors.

Technical Summary

• Payload Capacity: Up to 160 lbs (72.6 kg)
• Azimuth Range: 360°
• Elevation Range: ±95°
• Tracking Software: Two-line element (TLE) set program track
• Power: Power Over Ethernet (PoE)

Operational Use Cases

This positioner is utilized for automated satellite communications links requiring accurate pointing of directional antennas. Its TLE program track capability makes it highly suitable for tracking satellites in low earth orbit (LEO) and medium earth orbit (MEO).

Deployment Environments

The system is deployed in fixed site and tactical environments requiring automated target acquisition and sustained tracking of non-geostationary satellites.

Performance Metrics

• Supports payloads up to 160 lbs (72.6 kg)
• Offers full 360° azimuth coverage
• Provides ±95° of elevation range

Setup & Portability

Setup utilizes Power Over Ethernet (PoE) to minimize power and data cabling requirements. The embedded controller provides a full-featured web-based user interface for rapid configuration, manual control, and satellite database management.

Compatibility

• Optimized for pairing with 3-4 ft directional antennas
• Includes a command line interface for integration into larger hardware systems
• Compatible with an optional cross-elevation accessory to eliminate overhead tracking blind spots

FAQs

• What is the maximum payload capacity for this positioner? It supports directional antennas and payloads weighing up to 160 lbs (72.6 kg), typically accommodating 3-4 foot reflectors.
• How does two-line element set tracking work? Two-line element (TLE) tracking uses standardized orbital parameters to calculate and predict a satellite's path, enabling automated tracking of low or medium earth orbit objects.
• How is the keyhole effect mitigated during overhead passes? An optional cross-elevation accessory can be integrated with the system to provide continuous tracking and eliminate tracking blind spots directly overhead.
• 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

A demonstration video showing the web-based user interface and a simulated tracking sequence using TLE data for a LEO satellite pass would be highly beneficial.