US5654890A
Expired / Lapsed
US
⏱️ 0.0 years remaining
High resolution autonomous precision approach and landing system
Assignee: Winged Systems Corp
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Filing: 1994-05-31
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Granted: 1997-08-05
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Expires: 2014-05-31
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
2026-10-25 12:08
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: 30
Claim 1
Independent Claim
162 words
An approach and landing system for an aircraft, said system comprising: at least one navigation unit for providing navigation information; a low-bandwidth radar unit for providing radar information; a processor unit coupled to receive navigation information from said at least one navigation unit, and to receive radar information from said radar unit, said processor unit providing an output based on the provided navigation information and radar information; a memory, coupled to said processor unit, for storing information representing a scene, said processor unit correlating the stored scene information with the output of said processor unit to provide a mapped scene, said mapped scene comprising a real-time virtual view from said aircraft; a display unit, coupled to receive the output of said processor and coupled to said memory, for displaying said mapped scene for use in navigating said aircraft; and a steppable frequency oscillator for providing a signal which is stepped in frequency to said radar unit, thereby providing an increased range resolution.
Claim 2
Dependent Claim
162 words
An approach and landing system for an aircraft, said system comprising: at least one navigation unit for providing navigation information; a low-bandwidth radar unit for providing radar information; a processor unit coupled to receive navigation information from said at least one navigation unit, and to receive radar information from said radar unit, said processor unit providing an output based on the provided navigation information and radar information; a memory, coupled to said processor unit, for storing information representing a scene, said processor unit correlating the stored scene information with the output of said processor unit to provide a mapped scene, said mapped scene comprising a real-time virtual view from said aircraft; a display unit, coupled to receive the output of said processor and coupled to said memory, for displaying said mapped scene for use in navigating said aircraft; and a steppable frequency oscillator for providing a signal which is stepped in frequency to said radar unit, thereby providing an increased range resolution.
Claim 3
Dependent Claim
28 words
The approach and landing system as defined in claim 1, wherein said processor unit operates according to a Generalized Hough Transform map-match routine to provide the mapped scene.
Claim 4
Dependent Claim
26 words
The approach and landing system as defined in claim 1, wherein said signal provided by said oscillator to said radar unit is randomly stepped in frequency.
Claim 5
Dependent Claim
26 words
The approach and landing system as defined in claim 3, where said signal provided by said oscillator to said radar unit comprises a series of pulses.
Claim 6
Dependent Claim
37 words
The approach and landing system as defined in claim 4, wherein a first predetermined number of said pulses are randomly stepped in frequency so that each of said predetermined number of pulses is at a different frequency.
Claim 7
Dependent Claim
18 words
The approach and landing system as defined in claim 5, wherein the predetermined number of pulses is 160.
Claim 8
Dependent Claim
21 words
The approach and landing system as defined in claim 1, wherein a frequency step size of said oscillator is 250 KHz.
Claim 9
Dependent Claim
23 words
The approach and landing system as defined in claim 1, wherein said at least one navigation unit includes an Inertial Navigation System (INS).
Claim 10
Dependent Claim
23 words
The approach and landing system as defined in claim 1, wherein said at least one navigation unit includes a Global Positioning System (GPS).
Claim 11
Dependent Claim
33 words
The approach landing system as defined in claim 1, wherein said real-time virtual view is of sufficient accuracy to allow a pilot to fly said aircraft without an actual view from said aircraft.
Claim 12
Dependent Claim
33 words
The approach landing system as defined in claim 1, wherein said real-time virtual view is of sufficient accuracy to allow a pilot to land said aircraft without an actual view from said aircraft.
Claim 13
Independent Claim
139 words
A method of improving a range resolution of an aircraft approach and landing system including a low-bandwidth radar unit, the method comprising the steps of: generating a waveform which is stepped in frequency; applying the generated waveform to the radar unit in said approach and landing system to improve the range resolution of said radar unit; and using said radar unit to determine a resolution-improved range of said aircraft, said resolution improved range being of sufficient accuracy so that said approach and landing system is operable for at least one of automatically landing an aircraft without pilot intervention based on said resolution improved range and displaying a real-time virtual view from said aircraft of sufficient resolution range based on said resolution improved range to allow a pilot to safely land said aircraft without an actual view from said aircraft.
Claim 14
Independent Claim
139 words
A method of improving a range resolution of an aircraft approach and landing system including a low-bandwidth radar unit, the method comprising the steps of: generating a waveform which is stepped in frequency; applying the generated waveform to the radar unit in said approach and landing system to improve the range resolution of said radar unit; and using said radar unit to determine a resolution-improved range of said aircraft, said resolution improved range being of sufficient accuracy so that said approach and landing system is operable for at least one of automatically landing an aircraft without pilot intervention based on said resolution improved range and displaying a real-time virtual view from said aircraft of sufficient resolution range based on said resolution improved range to allow a pilot to safely land said aircraft without an actual view from said aircraft.
Claim 15
Dependent Claim
33 words
The method as defined in claim 12, wherein said generating step includes the step of randomizing the frequency steps so that the waveform applied to the radar unit is randomly stepped in frequency.
Claim 16
Dependent Claim
20 words
The method as defined in claim 13, wherein said generating step includes generating a series of pulses as the waveform.
Claim 17
Dependent Claim
28 words
The method as defined in claim 14, wherein a predetermined number of said pulses is randomly stepped in frequency so that each pulse is at a different frequency.
Claim 18
Dependent Claim
43 words
The method of improving a range resolution according to claim 12, further comprising the steps of: storing said generated wave form, receiving a signal into said radar unit, and using said generated wave form to decode said signal received by said radar unit.
Claim 19
Dependent Claim
34 words
The method of improving a range resolution of an aircraft according to claim 12, further comprising the step of using said determined range of said aircraft to automatically control the flight of said aircraft.
Claim 20
Dependent Claim
22 words
The method of improving a range resolution according to claim 17, wherein said step of automatically controlling includes automatically landing said aircraft.
Claim 21
Independent Claim
87 words
A method of improving a range resolution of an aircraft approach and landing system including a radar unit, the method comprising the steps of: generating a waveform which is stepped in frequency; applying the generated waveform to the radar unit in said approach and landing system to improve the range resolution of said radar unit; using said radar unit to determine a resolution-improved range of said aircraft; and displaying a virtual image representing a view from said aircraft, based at least in part on said resolution-improved range.
Claim 22
Independent Claim
87 words
A method of improving a range resolution of an aircraft approach and landing system including a radar unit, the method comprising the steps of: generating a waveform which is stepped in frequency; applying the generated waveform to the radar unit in said approach and landing system to improve the range resolution of said radar unit; using said radar unit to determine a resolution-improved range of said aircraft; and displaying a virtual image representing a view from said aircraft, based at least in part on said resolution-improved range.
Claim 23
Dependent Claim
156 words
An aircraft navigation system comprising: a plurality of control mechanisms for controlling the flight of an aircraft; a radar unit for providing radar information; means for providing a signal which is stepped in frequency to said radar unit to increase the range resolution of said radar unit so that said radar unit is operable for providing accurate representations of the earth-surface below said aircraft; a memory, coupled to said processor unit, for storing predetermined earth-surface information; a processor unit coupled to receive actual earth-surface information from said radar unit and said predetermined earth-surface information from said memory, said processor unit providing an output to at least one of said control mechanisms for automatically controlling the flight of said aircraft, said output based on the correlation between said stored predetermined earth-surface information and said actual earth-surface information, wherein said aircraft navigation system is operable for automatically flying said aircraft safely in near-land altitudes based on said output.
Claim 24
Dependent Claim
156 words
An aircraft navigation system comprising: a plurality of control mechanisms for controlling the flight of an aircraft; a radar unit for providing radar information; means for providing a signal which is stepped in frequency to said radar unit to increase the range resolution of said radar unit so that said radar unit is operable for providing accurate representations of the earth-surface below said aircraft; a memory, coupled to said processor unit, for storing predetermined earth-surface information; a processor unit coupled to receive actual earth-surface information from said radar unit and said predetermined earth-surface information from said memory, said processor unit providing an output to at least one of said control mechanisms for automatically controlling the flight of said aircraft, said output based on the correlation between said stored predetermined earth-surface information and said actual earth-surface information, wherein said aircraft navigation system is operable for automatically flying said aircraft safely in near-land altitudes based on said output.
Claim 25
Dependent Claim
44 words
The aircraft navigation system according to claim 20, further comprising a display unit, coupled to receive the output of said processor and coupled to said memory, for displaying an image based on the output of said processor and an image representing said earth-surface information.
Claim 26
Dependent Claim
24 words
The approach and landing system as defined in claim 20, wherein said signal is applied to said radar unit for both transmitting and receiving.
Claim 27
Dependent Claim
18 words
The aircraft navigation system according to claim 20, wherein said output is used to automatically control said aircraft.
Claim 28
Dependent Claim
18 words
The aircraft navigation system according to claim 23, wherein said output is used to automatically land said aircraft.
Claim 29
Dependent Claim
18 words
The aircraft navigation system as defined in claim 20, wherein said radar unit is a weather radar unit.
Claim 30
Dependent Claim
17 words
The aircraft navigation system as defined in claim 20, wherein said earth-surface information represents a specific location.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 2000-08-04 | 2001-02-03 | 2001-08-05 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2004-08-04 | 2005-02-03 | 2005-08-05 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2008-08-04 | 2009-02-03 | 2009-08-05 | $7700.00 | Window Closed / Lapsed |