Antenna Alignment Using Inertial Sensor Feedback

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Solution Overview

Problem

Existing antenna alignment techniques face challenges in accurately communicating signal strength differences and determining peak signal positions, leading to performance degradation due to misalignment, which is exacerbated by changes in antenna position over time, such as structural weaknesses or obstructions, and requires costly on-site technician visits.

Innovation Solution

Incorporating an accelerometer and gyroscope in the antenna to capture movement data, allowing for the detection of movement events and drift, and providing feedback for precise alignment, enabling the determination of angular position adjustments to achieve optimal signal strength and detect changes such as impacts or environmental factors like wind.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If traditional alignment techniques using signal strength feedback are used, then the alignment process can be performed without additional sensors, but the accuracy in determining peak signal position and communicating signal strength differences is insufficient

Engineering Contradiction:
Improvealignment accuracyVSAvoidsensor system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent replaces traditional signal-strength-based alignment feedback with an inertial measurement system using accelerometers and gyroscopes. The movement detection device captures accelerometer data and gyroscope data to determine angular position and movement events, substituting the mechanical signal strength measurement approach with an inertial sensing approach that directly measures physical movement and orientation.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent introduces an intermediary movement detection device that processes inertial sensor data to determine angular position and movement events. This intermediary layer translates raw accelerometer and gyroscope data into meaningful alignment information, bridging the gap between raw sensor measurements and actionable alignment feedback.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If alignment is performed during installation without movement detection, then the initial setup can be completed, but performance degradation occurs over time due to undetected position changes

Engineering Contradiction:
Improvealignment stabilityVSAvoidtime for on-site technician visits
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent implements continuous feedback by monitoring movement events and angular position changes over time. The system detects movement events using accelerometer data, determines angular position using gyroscope data, and provides feedback when the antenna moves from its aligned position. This continuous monitoring enables early detection of misalignment, allowing for timely corrections before significant performance degradation occurs.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent enables the antenna system to self-monitor its own alignment status through integrated inertial sensors. The movement detection device autonomously detects movement events, calculates angular position changes, and identifies when the antenna has drifted from its optimal position, eliminating the need for continuous external technician monitoring and enabling proactive maintenance.

Inventive Principle:
Principle #25Self-service

3Productivity

If misalignment is compensated by reducing modulation and coding rate, then data transmission can continue, but system resource usage increases to maintain the same data rate

Engineering Contradiction:
Improvedata rate maintenanceVSAvoidsystem resource usage
Core Design Contradiction:
ProductivityVSUse of energy by moving object

Solution Approach 1:

The patent performs preliminary detection of movement events and angular position changes before significant misalignment occurs. By continuously monitoring the antenna position using inertial sensors and detecting when the antenna moves from its aligned position, the system can alert operators to realign the antenna before performance degradation necessitates compensatory measures like reducing modulation and coding rate, thereby avoiding increased resource usage.

Inventive Principle:
Principle #10Preliminary action

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This solution enhances the accuracy and repeatability of antenna alignment, reduces operational costs by minimizing the need for on-site visits, and improves resource efficiency by maintaining data rate through accurate positioning and reduced redundancy.

Implementation Method 1

The antenna may include an accelerometer and a gyroscope that captures movement of the antenna

Methodology Applied
Scientific EffectAccelerometer: Accelerometer

Implementation Method 2

The antenna may include an accelerometer and a gyroscope that captures movement of the antenna

Methodology Applied
Scientific EffectGyroscope: Gyroscope

Data Source

PatentUS11699838B2Antenna with sensors for accurate pointing
Publication Date: 2023.07.11 VIASAT INC
  • US11699838B2 patent drawing
  • US11699838B2 patent drawing
  • US11699838B2 patent drawing

AI summary

Determining movement for alignment of a satellite antenna using accelerometer data and gyroscope data of the satellite antenna. Described techniques include receiving accelerometer data for a first time period from an accelerometer mounted on the antenna and analyzing the accelerometer data to determine a movement time window for a movement event of the antenna. The techniques may include receiving gyroscope data for the first time period from a gyroscope mounted on the antenna and analyzing the gyroscope data during the movement time window to determine an amount of movement of the antenna due to the movement event.