GNSS AND OPTICAL GUIDANCE AND MACHINE CONTROL
1 Assignment
0 Petitions
Accused Products
Abstract
A global navigation satellite sensor system (GNSS) and gyroscope control system for vehicle steering control comprising a GNSS receiver and antennas at a fixed spacing to determine a vehicle position, velocity and at least one of a heading angle, a pitch angle and a roll angle based on carrier phase position differences. The system also includes a control system configured to receive the vehicle position, heading, and at least one of roll and pitch, and configured to generate a steering command to a vehicle steering system. The system includes gyroscopes for determining system attitude change with respect to multiple axes for integrating with GNSS-derived positioning information to determine vehicle position, velocity, rate-of-turn, attitude and other operating characteristics. Relative orientations and attitudes between motive and working components can be determined using optical sensors and cameras. The system can also be used to guide multiple vehicles in relation to each other.
10 Citations
21 Claims
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1-12. -12. (canceled)
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13. A GNSS-based guidance system for a vehicle comprising a motive component and a working component interconnected by an articulated connection, which system comprises:
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a GNSS receiver mounted on said vehicle and configured for receiving GNSS ranging signals; a guidance computer on said motive component and connected to said receiver; first and second motive component antennas on said motive component and connected to said receiver; a fixed-distance, static baseline between said first and second motive component antennas; a variable-distance, moving baseline between said motive component and said working component, said moving baseline having variable distances corresponding to the orientations of said motive and working components in relation to each other; a prime inertial measuring unit (IMU) on said motive component configured for sending signal outputs to said guidance computer corresponding to roll (X), pitch (Y), and yaw (Z) movements of said motive component; an auxiliary IMU on said working component configured for sending signal outputs to said guidance computer corresponding to roll (X), pitch (Y), and yaw (Z) movements of said working component; optical targets on said working component configured for indicating roll (X), pitch (Y), and/or yaw (Z) directional misalignments of said working component in relation to the orientation of said motive component; and optical sensors on said motive component configured for detecting said optical targets, thus detecting roll (X), pitch (Y), and/or yaw (Z) directional misalignments of said working component in relation to the orientation of said motive component, and for sending signal outputs to said guidance computer. - View Dependent Claims (15, 16, 17, 18, 19, 21)
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14. (canceled)
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20. (canceled)
Specification