IMU Alignment with Mounting Structures Using CMM and Inclinometers

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Solution Overview

Problem

Existing calibration methods for inertial measurement units (IMUs) are insufficient for precise aerospace applications, where high accuracy in aligning IMU sensing axes with mounting structures is required.

Innovation Solution

The use of systems and methods that calibrate angular relationships between IMU sensing axes and mounting fixtures using advanced equipment such as coordinate measuring machines (CMM), inclinometers, and rate tables, determining rotation matrices to achieve precise alignment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If existing calibration methods are used, then the calibration process is simple, but the measurement precision and manufacturing precision are insufficient for aerospace applications

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

Solution Approach 1:

The calibration process is divided into distinct segments: (1) measuring fixture features with CMM to establish a fixture coordinate system, (2) measuring IMU features with CMM to establish an IMU coordinate system, and (3) calculating the rotation matrix from these two coordinate systems. This segmentation allows each step to be performed with appropriate precision using specialized equipment rather than requiring a single complex calibration system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces a fixture coordinate system as an intermediary reference frame between the IMU and the vehicle body. The CMM measures both the fixture features and IMU features relative to this common reference, enabling precise determination of the rotation matrix without requiring direct complex measurements between the IMU and vehicle body.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Manufacturing precision

If manufacturer calibration information is used, then the calibration process is straightforward, but the accuracy and precision are not sufficient for high-precision aerospace applications

Engineering Contradiction:
Improvealignment accuracyVSAvoidcalibration difficulty
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

The patent performs preliminary high-precision measurements of both the fixture features and IMU features using a CMM before the IMU is installed in the vehicle. This preliminary characterization creates accurate coordinate systems that can be used later without requiring complex on-site calibration procedures, thereby improving ease of manufacture while maintaining high precision.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent transforms the calibration problem from directly measuring angular relationships to measuring positions of multiple features in 3D space with a CMM. By changing the measurement parameters from direct angular measurements to positional measurements of multiple fiducial features, the system achieves higher precision through the CMM's positional accuracy while simplifying the overall calibration process.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS20250180375A1Alignment of inertial measurement units with mounting structures, and associated systems and methods
Publication Date: 2025.06.05 BLUE ORIGIN MANUFACTURING LLC
  • US20250180375A1 patent drawing
  • US20250180375A1 patent drawing
  • US20250180375A1 patent drawing

AI summary

Systems and methods for aligning inertial measurement units (IMUs) with mounting structures. A system can include fiducials attachable to a fixture, a coordinate measuring machine (CMM) for measuring positions of the fiducials, inclinometers attachable to the fixture, and a rate table for receiving the fixture and posing the fixture with the inclinometers and/or the IMUs. A method can include determining a first rotation matrix between a coordinate frame associated with the fiducials and a reference coordinate frame, determining a second rotation matrix between the reference coordinate frame and a coordinate frame associated with a rate table, determining a third rotation matrix between the coordinate frame associated with the rate table and a coordinate frame associated with an IMU, and multiplying the three rotation matrices by data from an IMU. The reference coordinate frame can be a coordinate frame associated with the fixture or associated with one or more inclinometers.