Inertial Measurement Unit for Aircraft
First Claim
1. A system for determining position of a vehicle, comprising:
- an integral inertial measurement unit (IMU) including a plurality of accelerometers and gyroscopes for providing raw data about movement of the vehicle;
a correction unit coupled to said IMU and arranged to receive or derive positional corrections and the raw data from said IMU and generate accurate positional information about the vehicle based on the raw data and positional corrections; and
a navigation system coupled to said correction unit for receiving and acting upon the accurate positional information of the vehicle provided by said correction unit.
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Accused Products
Abstract
System for determining position of a vehicle includes an integral inertial measurement unit (IMU) including accelerometers and gyroscopes for providing raw data about movement of the vehicle and a correction unit coupled to the IMU and arranged to receive and/or derive positional corrections and the raw data from the IMU and generate accurate positional information about the vehicle based on the raw data and positional corrections. A navigation system is coupled to the correction unit and receives and acts upon the positional information of the vehicle provided by the correction unit. The IMU may be a MEMS-packaged IMU and integrated with the correction unit in combination with one another. A map database may be coupled to the navigation system which would receive information about a travel lane the vehicle is travelling on and could guide an operator of the vehicle based on the accurate positional information and travel lane information.
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Citations
20 Claims
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1. A system for determining position of a vehicle, comprising:
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an integral inertial measurement unit (IMU) including a plurality of accelerometers and gyroscopes for providing raw data about movement of the vehicle; a correction unit coupled to said IMU and arranged to receive or derive positional corrections and the raw data from said IMU and generate accurate positional information about the vehicle based on the raw data and positional corrections; and a navigation system coupled to said correction unit for receiving and acting upon the accurate positional information of the vehicle provided by said correction unit. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
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14. A system for determining position of an aircraft, comprising:
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a single integrated unit including a MEMS-packaged integral inertial measurement unit (IMU) and a correction unit coupled to said IMU, said IMU including a plurality of accelerometers and gyroscopes for providing raw data about movement of the vehicle, said correction unit being arranged to receive or derive positional corrections and the raw data from said IMU and generate accurate positional information about the vehicle based on the raw data and positional corrections; and a navigation system coupled to said correction unit for receiving and acting upon the accurate positional information of the vehicle provided by said correction unit. - View Dependent Claims (15, 16, 17, 18, 19, 20)
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Specification