Terrain referenced navigation-Schuler cycle error reduction method and apparatus
First Claim
1. A Schuler cycle phase detection method, wherein the Schuler cycle has at least one Schuler cycle precision point, the Schuler cycle phase detection method comprising the steps of:
- (a) determining a location of the at least one Schuler cycle precision point at at least one predetermined point in the Schuler cycle by relating the Schuler cycle to a predetermined cyclic measurement that varies with the Schuler cycle, and relating the Schuler cycle precision point to the predetermined cyclic measurement; and
(b) estimating a current Schuler cycle phase from the at least one Schuler cycle precision point.
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Abstract
A method for Schuler cycle error reduction is provided for use in a terrain referenced navigation system. Terrain Reference Navigation filter coefficients are analytically determined using a terrain reference navigation database and a hypothetical Schuler cycle. The optimum filter coefficients are determined assuming that there will be three parallel filters being executed during flight. The first filter is a nominal filter which represents a compromise between sensing zero crossing of a Schuler cycle error and peak changes of a Schuler cycle. The other filters are chosen to be perpendicular to the instantaneous line of flight. One is a peak filter, the other is a zero crossing filter. The peak filter is set to capture the inertial navigation unit when the Schuler cycle is changing rapidly. The zero crossing detector is set to capture the inertial navigation unit when it is zero crossing. The Schuler cycle is detected by algebraically noting similar features of each filter. INS measurements are then dynamically compensated for the now known Schuler cycle.
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Citations
22 Claims
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1. A Schuler cycle phase detection method, wherein the Schuler cycle has at least one Schuler cycle precision point, the Schuler cycle phase detection method comprising the steps of:
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(a) determining a location of the at least one Schuler cycle precision point at at least one predetermined point in the Schuler cycle by relating the Schuler cycle to a predetermined cyclic measurement that varies with the Schuler cycle, and relating the Schuler cycle precision point to the predetermined cyclic measurement; and (b) estimating a current Schuler cycle phase from the at least one Schuler cycle precision point.
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2. A Schuler cycle error reduction method for a terrain referenced navigation system, wherein the terrain referenced navigation system contains navigation errors according to the Schuler cycle and wherein the Schuler cycle has at least one Schuler cycle precision point, the Schuler cycle error reduction method comprising the steps of:
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(a) determining a location of the at least one Schuler cycle precision point at at least one predetermined point in the Schuler cycle by relating the Schuler cycle to a predetermined cyclic measurement that varies with the Schuler cycle, and relating the Schuler cycle precision point to the predetermined cyclic measurement; (b) estimating a Schuler cycle phase from the at least one Schuler cycle precision point; and (c) compensating the terrain referenced navigation system for the navigation errors according to the Schuler cycle. - View Dependent Claims (3, 4, 5, 6, 7, 8)
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9. A Schuler cycle phase detection method for a Schuler cycle, wherein the method comprises the steps of:
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(a) determining a cyclic function having a cyclic phase, wherein the cyclic function phase relates to the Schuler cycle phase; (b) determining at least one point of the Schuler cycle that corresponds to at least one point of the cyclic function; and (c) determining the Schuler cycle phase from the cyclic function phase.
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10. A Schuler cycle error reduction method for a terrain referenced navigation system wherein the terrain referenced navigation system contains navigation errors according to the Schuler cycle, wherein the Schuler cycle has at least one Schuler cycle precision point, the Schuler cycle error reduction method comprising the steps of:
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(a) determining a cyclic function having a cyclic phase, wherein the cyclic function phase relates to the Schuler cycle phase; (b) determining at least one point of the Schuler cycle that corresponds to at least one point of the cyclic function; (c) determining the Schuler cycle phase from the cyclic function phase; and (d) compensating the terrain referenced navigation system for the navigation errors according to the Schuler cycle. - View Dependent Claims (11, 12, 13, 14, 15, 16, 17, 18)
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19. An analytical method performed on a computer for determining the value of a predetermined error model for a terrain reference navigation system comprising the steps of:
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(a) setting a terrain reference navigation filter coefficient to a nominal model filter; (b) analyzing an existing predetermined terrain reference navigation data base from a simulated terrain reference navigation flight; (c) running a predetermined number of test cases on a flight path of a hypothetical aircraft running through the predetermined terrain referenced navigation data base; (d) storing flight profiles; (e) analyzing different Q values ranging from a very small predetermined value to a very large predetermined value; (f) imposing an artificial Schuler cycle on the flight path during each run; (g) determining the Schuler cycle error based on prior knowledge of the location of the Schuler cycle; and (h) determining the values of Q for any predetermined rate of change based on the known error models for the multitude of cases. - View Dependent Claims (20, 21, 22)
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Specification