Patent US6018698A successfully refreshed from Google Patents.
US6018698A
Expired / Lapsed
US
⏱️ 0.0 years remaining
High-precision near-land aircraft navigation system
Assignee: Winged Systems Corp
•
Filing: 1997-06-23
•
Granted: 2000-01-25
•
Expires: 2017-06-23
Abstract
Abstract An aircraft including an approach and landing system, including a navigation unit for providing navigation information, a weather radar unit for providing radar information, a processor which receives navigation information from the navigation unit and information from the weather radar unit, the processor unit providing an output representing information concerning the aircraft in accordance with the provided navigation information and radar information, a memory for storing information representing a scene, the processor unit correlating the stored scene information with the output representing information concerning the aircraft to provide a mapped scene, a display unit for displaying the output of said processor and the mapped scene, and a steppable frequency oscillator for providing a signal which is stepped in frequency to the weather radar unit, thereby providing an increased range resolution.
Inventors
- 👤 Joseph M. Nicosia
- 👤 Keith R. Loss
- 👤 Gordon A. Taylor
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 22:02
CPC Classifications
G; G08; G08G; G08G5/00; G08G5/20; G08G5/21; G01; G01C; G01C21/00; G01C21/10; G01C21/12; G01C21/16; G01C21/165; G01C21/1652; G01C23/00; G01C23/005; G01S; G01S13/00; G01S13/02; G01S13/06; G01S13/08; G01S13/10; G01S13/26; G01S13/28; G01S13/284; G01S13/286; G01S13/88; G01S13/91; G01S13/913; G01S13/95; G01S13/953; G01S19/00; G01S19/01; G01S19/13; G01S19/14; G01S19/15; G01S7/00; G01S7/02; G01S7/41; G01S7/411; G01S7/412; G05; G05D; G05D1/00; G05D1/04; G05D1/06; G05D1/0607; G05D1/0653; G05D1/0676; G08G5/50; G08G5/52; G08G5/54; G08G5/55; G08G5/70; G08G5/74; G08G5/76; G01S13/86; G01S13/89; G01S13/90; G01S19/38; G01S19/39; G01S19/52; Y; Y02; Y02A; Y02A90/00; Y02A90/10
Claims Analysis
Total Claims: 14
Claim 1
Independent Claim
122 words
A method of aircraft navigation using radar, comprising: storing information of cultural or natural features in an area of the ground along and to the sides of a flight path; using said radar during flight to obtain information of said features along and to the sides of said flight path; comparing said stored information with said information obtained by radar to determine successive different match points representing different ground locations; determining the range and range rate of each of said match points; determining the aircraft's location and velocity based on repetitive range and range rate measurements of said match points; and supplementing the accuracy of said aircraft location and velocity determination with information from at least one of an additional navigation unit.
Claim 2
Independent Claim
122 words
A method of aircraft navigation using radar, comprising: storing information of cultural or natural features in an area of the ground along and to the sides of a flight path; using said radar during flight to obtain information of said features along and to the sides of said flight path; comparing said stored information with said information obtained by radar to determine successive different match points representing different ground locations; determining the range and range rate of each of said match points; determining the aircraft's location and velocity based on repetitive range and range rate measurements of said match points; and supplementing the accuracy of said aircraft location and velocity determination with information from at least one of an additional navigation unit.
Claim 3
Dependent Claim
19 words
The method according to claim 1, wherein said additional navigation unit information is based upon integration of inertial measurements.
Claim 4
Dependent Claim
32 words
The method according to claim 1, wherein said additional navigation unit information represents locations between said match points and is combined with said aircraft location and velocity determination using Kalman statistical filtering.
Claim 5
Dependent Claim
84 words
The method according to claim 1, wherein a phase changing effect created by motion of said navigation unit is reduced, said method comprising: defining subsets of a frequency hopped radar signal and a center frequency for each subset, bouncing said radar signal off of an object and receiving a reflected version of said signal to determine a phase change in said signal; receiving reflected versions of said subsets, and subtracting phase effects from the samples that correspond to the center frequency of said subset.
Claim 6
Dependent Claim
74 words
The method of claim 1 wherein phase compensation is provided for said radar, said method comprising: storing a pseudo-random frequency order; changing a transmission frequency of a radar signal based on said pseudo-random frequency order; using said pseudo-random frequency order to sample a received radar signal which is a reflected version of said transmitted radar signal, thereby generating samples of said received radar signal; and reordering said samples in an order of increasing frequency.
Claim 7
Dependent Claim
29 words
The method according to claim 5, further comprising: summing a group of said samples; and performing an Inverse Digital Fourier Transform on said samples to develop a range value.
Claim 8
Dependent Claim
135 words
The method according to claim 5, further comprising: tagging said received samples with information of their order of reception and order of frequency; identifying a coarse range of interest based on a particular area of the ground; selecting the received samples which correspond to said particular area; defining signal subsets of said transmitted signal; determining the Doppler frequencies for said selected samples and center frequencies for the subsets corresponding to said particular area; arranging said received samples in frequency order within said subsets; calculating the phase rotation due to transmit frequencies and receive times for the received samples, and subtracting said phase rotations from the corresponding samples according to the time order and wavelength of said sample, to thereby reduce effects of motion of the navigation unit on the interpretation of the received radar signals.
Claim 9
Independent Claim
95 words
A method of aircraft navigation using radar, comprising: storing information of cultural or natural features in an area of the ground along and to the sides of a flight path; using said radar during flight to obtain information of said features along and to the sides of said flight path; comparing said stored information with said information obtained by radar to determine match points representing different ground locations; determining the range and range rate of said match points; and using said range and range rate in the navigation or state vector measurements of said aircraft.
Claim 10
Independent Claim
95 words
A method of aircraft navigation using radar, comprising: storing information of cultural or natural features in an area of the ground along and to the sides of a flight path; using said radar during flight to obtain information of said features along and to the sides of said flight path; comparing said stored information with said information obtained by radar to determine match points representing different ground locations; determining the range and range rate of said match points; and using said range and range rate in the navigation or state vector measurements of said aircraft.
Claim 11
Dependent Claim
84 words
A method according to claim 8 wherein a phase changing effect created by motion of said navigation unit is reduced, said method comprising: defining subsets of a frequency hopped radar signal and a center frequency for each subset, bouncing said radar signal off of an object and receiving a reflected version of said signal to determine a phase change in said signal; receiving reflected versions of said subsets, and subtracting phase effects from the samples that correspond to the center frequency of said subset.
Claim 12
Dependent Claim
74 words
The method of claim 8 wherein phase compensation is provided for said radar, said method comprising: storing a pseudo-random frequency order; changing a transmission frequency of a radar signal based on said pseudo-random frequency order; using said pseudo-random frequency order to sample a received radar signal which is a reflected version of said transmitted radar signal, thereby generating samples of said received radar signal; and reordering said samples in an order of increasing frequency.
Claim 13
Dependent Claim
29 words
The method according to claim 10, further comprising: summing a group of said samples; and performing an Inverse Digital Fourier Transform on said samples to develop a range value.
Claim 14
Dependent Claim
135 words
The method according to claim 10, further comprising: tagging said received samples with information of their order of reception and order of frequency; identifying a coarse range of interest based on a particular area of the ground; selecting the received samples which correspond to said particular area; defining signal subsets of said transmitted signal; determining the Doppler frequencies for said selected samples and center frequencies for the subsets corresponding to said particular area; arranging said received samples in frequency order within said subsets; calculating the phase rotation due to transmit frequencies and receive times for the received samples, and subtracting said phase rotations from the corresponding samples according to the time order and wavelength of said sample, to thereby reduce effects of motion of the navigation unit on the interpretation of the received radar signals.
References Cited (Backward Citations)
US3715753A
Cited
US3416752A
Cited
US4106726A
Cited
US3775766A
Cited
US4194204A
Cited
US4103300A
Cited
US4241345A
Cited
US4495580A
Cited
US4429312A
Cited
US4562439A
Cited
US4631541A
Cited
US4646244A
Cited
US4910674A
Cited
US4698635A
Cited
US4768156A
Cited
US4866450A
Cited
US5111400A
Cited
US4851848A
Cited
US4891762A
Cited
US4914734A
Cited
US5136297A
Cited
US5227801A
Cited
US5428361A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 2003-01-24 | 2003-07-26 | 2004-01-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2007-01-24 | 2007-07-26 | 2008-01-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2011-01-24 | 2011-07-26 | 2012-01-25 | $7700.00 | Window Closed / Lapsed |