INERTIAL NAVIGATION UNIT ENHACED WITH ATOMIC CLOCK
An atomic clock is used in conjunction with the GNSS receiver and the inertial sensors, creating a more capable inertial navigation system (INS). The system is composed of a GNSS receiver, an accurate clock, and a mechanism for measuring relative pose changes. The system being presented utilizes an inertial measurement unit (IMU) to provide the relative pose changes, but other mechanisms can be used—like visual and ladar odometry. The GNSS receiver measures the pseudo-ranges to the GNSS satellites in the field of view. These measurements are “time tagged” with the accuracy of the atomic clock. The relative motion between the pseudo-ranges is measured using the IMU. Finally, the lock is achieved by filtering these measurements. The filtering mechanism can vary, from the traditional Kalman Filters to other mechanisms that attempt to minimize the mean square error.
1 . The device providing absolute and relative localization, composed of:
a computer system for receiving and time-tagging pseudo-ranges from one or more Global Navigation Satellite Systems (GNSS);
an accurate clock;
a relative localization system that can measure the change in pose between subsequent GNSS measurements; and
a filtering mechanism that can solve to find position.
2 . The device of claim 1 , comprising
a different filtering mechanism that utilizes the pseudo-ranges and carrier phase measurements to improve on the relative positioning.
3 . The device of claim 1 , using the clock and possible skews to detect spoofing.
4 . The device of claim 1 , further comprising of
visual odometry or ladar odometry, to provide relative localization between GNSS measurements.
5 . The device of claim 1 , further comprising
an external relative of absolute position measurement.
6 . The device of claim 5 , wherein the external relative of absolute position measurement is taken from a barometer, inclinometer, or compass.
7 . The device of claim 1 , wherein the GNSS receiver and the clock are implemented as a single device.
8 . The device of claim 1 , using measurements from another vehicle to calculate the relative position between vehicles using a differential GNSS filtering mechanism.
9 . The device of claim 1 , wherein
the absolute time in two systems or vehicles is used to provide a GNSS lock.
10 . The device of claim 9 , wherein
the relative position between the two or more vehicles is measured directly or indirectly using visual or LADAR matching.
11 . The device of claim 1 , wherein
the onboard clock is adjusted to absolute time using a lock from the satellites.
12 . The device of claim 11 , wherein the onboard clock is adjusted to absolute time using a lock from the satellites when all satellites are seen at the same time, or when the satellites are seen sequentially.
13 . The device of claim 1 , further comprising
using two or more satellites on the GNSS from different sources, in combination, to get a fix.
14 . The device of claim 1 , further comprising the capability of determining an objects orientation.
15 . The device of claim 1 , wherein the one or more GNSS sources is selected from a Global Positioning System (GPS), GLONASS, and GALILEO.
16 . The device of claim 1 , wherein the clock is an atomic clock.
17 . An inertial navigation system (INS) comprising:
a GNSS receiver;
an atomic clock; and
a mechanism for measuring relative pose changes;
utilizing an inertial measurement unit (IMU) to provide the relative pose changes;
the GNSS receiver measures the pseudo-ranges to the GNSS satellites in the field of view;
these measurements are time tagged with the accuracy of the atomic clock;
the relative motion between the pseudo-ranges is measured using the IMU;
the lock is achieved by filtering these measurements.
18 . The device of claim 1 , wherein visual and ladar odometry are used to provide the relative pose changes.
19 . The device of claim 1 , wherein the filtering mechanism is a Kalman Filter to minimize the mean square error.