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Proceedings ArticleDOI

GPS Align In Motion of civilian strapdown INS

TLDR
Align In Motion as mentioned in this paper allows initialization of a Strapdown inertial navigation system while an aircraft is moving, in the air or on the ground, using a GPS and an inertial reasonableness test.
Abstract
Strapdown inertial navigation systems require an initialization process that establishes the relationship between the aircraft body frame and the local geographic reference. This process, called alignment, generally requires the device to remain stationary for some period of time in order to establish this initial state. This paper describes an alignment process where the initialization occurs while the device is moving. This is possible because an accurate determination of the aircraft motion is available based on measurements obtained from GPS. Align In Motion allows initialization of a Strapdown Inertial Navigation System while an aircraft is moving, in the air or on the ground. This is accomplished using Civilian grade GPS and an inertial reasonableness test, thereby allowing commercial data integrity requirements to be met. Align In Motion has been FAA certified to recover pure INS performance equivalent to stationary align procedures for civilian flight times up to 18 hours. This Align In Motion capability allows the removal of dedicated backup batteries on aircraft resulting in weight, cost, and reliability improvements. Align In Motion also has benefits for aircraft operations on the ground, on board ship, and in the air such as reduced turn backs, quicker dispatch, and world-wide alignment including polar regions. This paper will describe an avionics architecture using Align In Motion. It will cover INS warm start and cold start following a power interrupt with recovery to full inertial navigation capability without pilot interaction. Successful flight test results will also be presented.

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Citations
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Journal ArticleDOI

Velocity/Position Integration Formula Part I: Application to In-Flight Coarse Alignment

TL;DR: An optimization-based coarse alignment approach that uses GPS position/velocity as input, founded on the newly-derived velocity/position integration formulae is proposed, and can serve as a nice coarse in-flight alignment without any prior attitude information for the subsequent fine Kalman alignment.
Journal ArticleDOI

Real-time accurate odometer velocity estimation aided by accelerometers

TL;DR: In this article, the effect of the noise of odometer velocity on in-motion alignment accuracy is presented, based on the strap-down gyro-compass algorithm, and a velocity tracking model is designed as the state model, to describe the relationship between and among the vehicle's velocity, acceleration and jerk in the vehicle frame.
Proceedings ArticleDOI

On-the-move alignment for strap-down inertial navigation system

TL;DR: The initial alignment of the terrestrial vehicle borne strap-down inertial navigation system (SINS) is investigated and an on-the-move alignment algorithm using the information provided by an odometer, whose scale factor may have an unknown constant bias, is proposed.
Proceedings Article

Automatic calibration and in-motion alignment of an odometer-aided INS

TL;DR: In this article, the problem of odometer-aided in-motion alignment is investigated, where the nonholonomic constraints are efficiently employed in the designed Kalman filtering process with the measured data provided by a calibrated odometer.
Patent

Multiple truth reference system and method

TL;DR: In this article, a system comprises a plurality of reference navigation systems, each reference navigation system configured to generate a respective reference navigation solution, and a processing unit configured to compare the test navigation solution to each of the respective reference navigations to estimate one or more errors in the differences between the test navigations and the respective navigation solutions.
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