Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle
Reexamination Certificate
1998-05-08
2001-04-17
Cuchlinski, Jr., William A. (Department: 3661)
Data processing: vehicles, navigation, and relative location
Vehicle control, guidance, operation, or indication
Aeronautical vehicle
C073S17800T, C073S17800T, C340S970000, C701S301000
Reexamination Certificate
active
06219592
ABSTRACT:
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to a terrain awareness system (TAS) and more particularly to a system for alerting a pilot of an aircraft of a dangerous flight condition which monitors the position as well as the trajectory of an aircraft based upon a satellite-based navigation system, such as a global positioning system (GPS), to provide a LOOK-AHEAD/LOOK-DOWN as well as LOOK-UP terrain advisory and warning indications based upon stored terrain data which provides relatively longer warning times than known ground proximity warning systems while minimizing nuisance warnings.
2. Description of the Prior Art
Various systems are known in the art that provide warnings and advisory indications of hazardous flight conditions. Among such systems are systems generally known as ground proximity warning systems (GPWS) which monitor the flight-conditions of an aircraft and provide a warning if flight conditions are such that inadvertent contact with terrain is imminent. Among the flight conditions normally monitored by such systems are radio altitude and rate, barometric altitude and rate, air speed, flap and gear positions. These parameters are monitored and an advisory signal and/or warning signal is generated when the relationship between the parameters is such that terrain impact is likely to occur. Typical examples of such systems are disclosed in U.S. Pat. Nos. 3,715,718; 3,936,796; 3,958,218; 3,944,968; 3,947,808; 3,947,810; 3,934,221; 3,958,219; 3,925,751; 3,934,222; 4,060,793; 4,030,065; 4,215,334; and 4,319,218, all assigned to the same assignee as the assignee of the present invention and hereby incorporated by reference.
While the above-referenced systems do provide advisory and warning signals in the event of proximity to terrain, the warnings generated by such systems are based solely upon flight conditions of the aircraft and do not utilize any navigational information. Consequently, the sensitivity of such systems must be adjusted to provide adequate warnings when a hazardous flight condition exists without generating false or spurious warnings. However, such an adjustment can result in a compromise that may still result in nuisance warnings over terrain unique to particular geographic areas and shorter than desired warning times in yet other geographic areas.
Several attempts have been made to improve upon such ground proximity warning systems utilizing ground-based navigational information. For example, U.S. Pat. Nos. 4,567,483; 4,646,244; 4,675,823; and 4,914,436 all disclose ground proximity warning systems which monitor the position of the aircraft relative to stored terrain data in order to provide modified ground proximity warnings. However, the utility of such systems is limited. For example, the systems disclosed in U.S. Pat. Nos. 4,567,483 and 4,914,436 disclose ground proximity warning systems which utilize navigational data to modify predetermined warning envelopes surrounding certain particular airports.
U.S. Pat. Nos. 4,646,244 and 4,675,823 disclose terrain advisory systems which utilize various ground-based navigational inputs and stored terrain data to provide various ground proximity warning systems based on the position of the aircraft. In order to conserve memory, the terrain data is modeled in various geometric shapes as a function of the elevation of the terrain within the area defined by the geometric shape- The warning signals are generated as a function of the position of the aircraft relative to the model. While such systems do provide adequate terrain warnings, such systems may cause nuisance warnings under certain conditions since the predicted trajectory of the aircraft is not taken into consideration.
Another problem with such systems is that they are based upon ground-based navigational systems, such as VOR/DME and LORAN. Such ground-based navigational systems are being replaced with relatively more accurate satellite systems, such as the global positioning system (GPS). Moreover, such ground-based systems are only able to provide two-dimensional position data. Thus, with such systems, the altitude of the aircraft must be supplied by an auxiliary device, such as an altimeter, which increases the complexity of the system as well as the cost.
SUMMARY OF THE INVENTION
It is an object of the present invention to solve various problems associated with the prior art.
It is yet another object of the present invention to provide a terrain awareness system which provides increased warning times to the pilot of an aircraft of a hazardous flight condition while minimizing nuisance warnings.
It is yet another object of the present invention to provide a system which provides a LOOK-AHEAD/LOOK-DOWN as well as a LOOK-UP terrain advisory and warning indications to the pilot of an aircraft of a hazardous flight condition based upon the predicted trajectory of the aircraft.
It is yet another object of the present invention to provide a terrain awareness system which utilizes inputs from a satellite-based navigation system, such as the global positioning system (GPS).
Briefly, the present invention relates to a terrain awareness system (TAS) which provides LOOK-AHEAD/LOOK-DOWN as well as LOOK-UP terrain advisory and warning indications to the pilot of an aircraft of a hazardous flight condition. The TAS includes an airport data base as well as a terrain data base that is structured to provide various resolutions depending on the topography of the particular geographic area of interest. Navigational data from a satellite-based navigation system, such as a global positioning system (GPS), is used to provide a LOOK-AHEAD/LOOK-DOWN and LOOK-UP terrain advisory and terrain warning indications based upon the current position and projected flight path of the aircraft. Since the terrain advisory and the warning signals are a function of the flight path of the aircraft,,nuisance warnings are minimized.
REFERENCES:
patent: 3715718 (1973-02-01), Astengo
patent: 3925751 (1975-12-01), Bateman et al.
patent: 3934221 (1976-01-01), Bateman et al.
patent: 3934222 (1976-01-01), Bateman et al.
patent: 3936796 (1976-02-01), Bateman et al.
patent: 3944968 (1976-03-01), Bateman et al.
patent: 3947808 (1976-03-01), Bateman
patent: 3947810 (1976-03-01), Bateman et al.
patent: 3958218 (1976-05-01), Bateman
patent: 3958219 (1976-05-01), Bateman
patent: 4030065 (1977-06-01), Bateman
patent: 4060793 (1977-11-01), Bateman
patent: 4063073 (1977-12-01), Strayer
patent: 4215334 (1980-07-01), Bateman
patent: 4224669 (1980-09-01), Brame
patent: 4319218 (1982-03-01), Bateman
patent: 4484192 (1984-11-01), Seitz et al.
patent: 4567483 (1986-01-01), Bateman et al.
patent: 4642775 (1987-02-01), Cline et al
patent: 4646244 (1987-02-01), Bateman et al.
patent: 4675823 (1987-06-01), Noland
patent: 4835537 (1989-05-01), Manion
patent: 4894655 (1990-01-01), Joguet et al.
patent: 4903212 (1990-02-01), Yokouchi et al.
patent: 4912645 (1990-03-01), Kakihara et al.
patent: 4914436 (1990-04-01), Bateman et al.
patent: 4914733 (1990-04-01), Gralnick
patent: 4916448 (1990-04-01), Thor
patent: 4924401 (1990-05-01), Bice et al.
patent: 4947164 (1990-08-01), Bateman
patent: 4954959 (1990-09-01), Moroto et al.
patent: 4987413 (1991-01-01), Grove
patent: 5086396 (1992-02-01), Waruszewski, Jr.
patent: 5136512 (1992-08-01), Le Borne
patent: 5140532 (1992-08-01), Beckwith, Jr. et al.
patent: 5153588 (1992-10-01), Muller
patent: 5155688 (1992-10-01), Tanaka et al.
patent: 5157615 (1992-10-01), Brodegard
patent: 5196847 (1993-03-01), Bateman
patent: 5202690 (1993-04-01), Frederick
patent: 5220322 (1993-06-01), Bateman et al.
patent: 5252978 (1993-10-01), Priestley
patent: 5257195 (1993-10-01), Hirata
patent: 5265025 (1993-11-01), Hirata
patent: 5285391 (1994-02-01), Smith, Jr. et al.
patent: 5293163 (1994-03-01), Kakihara et al.
patent: 5293318 (1994-03-01), Fukushima
patent: 5337242 (1994-08-01), Yamamoto et al.
patent: 5414631 (1995-05-01), Denoize et al.
patent: 5442556 (1995-08-01), Boyes et al.
patent: 5486821 (1996-01-01), Stevens et al.
patent: 5488563 (1996
Conner Kevin J.
Johnson Steven C.
Muller Hans R.
Allied-Signal Inc.
Cuchlinski Jr. William A.
Pipala Edward
LandOfFree
Method and apparatus for terrain awareness does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Method and apparatus for terrain awareness, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method and apparatus for terrain awareness will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-2439022