IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0174607
(2005-07-06)
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등록번호 |
US-7453375
(2008-11-18)
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발명자
/ 주소 |
- Chamas,Bassam H.
- Yokota,Ryuichi
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출원인 / 주소 |
- Toyota Motor Sales, U.S.A. Inc.
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대리인 / 주소 |
Finnegan, Henderson, Farabow, Garrett & Dunner, LLP
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인용정보 |
피인용 횟수 :
11 인용 특허 :
29 |
초록
▼
Methods and apparatus are provided for airspace navigation. Airspace navigation information for an aircraft is displayed in a first mode, such as, in a horizontal mode. One or more navigation events may then be detected, such as, proximity to a terrain feature, weather, traffic etc. The airspace na
Methods and apparatus are provided for airspace navigation. Airspace navigation information for an aircraft is displayed in a first mode, such as, in a horizontal mode. One or more navigation events may then be detected, such as, proximity to a terrain feature, weather, traffic etc. The airspace navigation information for the aircraft is then displayed using dual modes, e.g., a horizontal mode and a vertical mode. Display parameters, such as colors, resolution, distance, scale, etc. may be set automatically or by a user. The display may also include information, such as avionics systems information, and communications information.
대표청구항
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What is claimed is: 1. A navigation system for an aircraft having a top and at least one side, the system comprising: a navigation data module to receive navigation data; a display to display the navigation data in a horizontal mode; and a controller to detect a navigation event based on the naviga
What is claimed is: 1. A navigation system for an aircraft having a top and at least one side, the system comprising: a navigation data module to receive navigation data; a display to display the navigation data in a horizontal mode; and a controller to detect a navigation event based on the navigation data and to cause the display to automatically display the navigation data in the horizontal mode and a vertical mode, in response to the navigation event, wherein the vertical mode includes a vertical mode aircraft symbol and the horizontal mode includes a horizontal mode aircraft symbol, the vertical mode includes lines showing gradations of altitude, the horizontal mode displays a top view of the aircraft together with a top view of Federal Aviation Administration (FAA)-defined airspace near the aircraft, the top view being from a substantially top perspective, and the vertical mode displays a side view of the aircraft together with a side view of the FAA-defined airspace near the aircraft, the side view being from a substantially side perspective, the horizontal mode displays the top view of the aircraft together with a top view of terrain near the aircraft, the top view being from a substantially top perspective, and the vertical mode displays the side view of the aircraft together with a side view of the terrain near the aircraft, the side view being from a substantially side perspective, the horizontal mode displays the top view of the aircraft together with a top view of weather near the aircraft, the top view being from a substantially top perspective, and the vertical mode displays the side view of the aircraft together with a side view of weather near the aircraft, the side view being from a substantially side perspective, the horizontal mode displays the top view of the aircraft together with a top view of terrain near the aircraft, the top view being from a substantially top perspective, and the vertical mode displays the side view of the aircraft together with a side view of other aircraft near the aircraft, the side view being from a substantially side perspective, and the horizontal mode displays the top view of the aircraft together with a top view of an instrument landing system (ILS) approach path including a localizer center beam and a localizer pattern, the top view being from a substantially top perspective, and the vertical mode displays the side view of the aircraft together with a side view of the ILS approach path including a glide slope center beam and a glide slope pattern, the side view being from a substantially side perspective. 2. The system of claim 1, wherein the navigation data module receives global positioning system signals. 3. The system of claim 1, wherein the navigation data module receives data indicating weather including a wind feature. 4. The system of claim 1, wherein the navigation data module receives data from an avionics system of the aircraft. 5. The system of claim 1, wherein the navigation data module receives data from a communications system of the aircraft. 6. The system of claim 1, wherein the navigation data module receives data from a computer readable medium. 7. The system of claim 1, wherein the navigation data module receives data from a network. 8. The system of claim 1, wherein the FAA-defined airspace is one of restricted airspace, class B airspace, class C airspace, and class D airspace. 9. The system of claim 1, further comprising an indication module that provides a voice warning. 10. The system of claim 9, wherein the voice warning is provided in response to one of the FAA-defined airspace, weather, terrain, and other aircraft. 11. A navigation system for an aircraft having a top and at least one side, the system comprising: a navigation data module to receive navigation data; a display to display the navigation data in a vertical mode; and a controller to detect a navigation event based on the navigation data and to cause the display to automatically display the navigation data in the vertical mode and a horizontal mode, in response to the navigation event, wherein the vertical mode includes a vertical mode aircraft symbol and the horizontal mode includes a horizontal mode aircraft symbol, the vertical mode includes lines showing gradations of altitude, the horizontal mode displays a top view of the aircraft together with a top view of Federal Aviation Administration (FAA)-defined airspace near the aircraft, the top view being from a substantially top perspective, and the vertical mode displays a side view of the aircraft together with a side view of the FAA-defined airspace near the aircraft, the side view being from a substantially side perspective, the horizontal mode displays the top view of the aircraft together with a top view of terrain near the aircraft, the top view being from a substantially top perspective, and the vertical mode displays the side view of the aircraft together with a side view of the terrain near the aircraft, the side view being from a substantially side perspective, the horizontal mode displays the top view of the aircraft together with a top view of weather near the aircraft the top view being from a substantially top perspective, and the vertical mode displays the side view of the aircraft together with a side view of weather near the aircraft, the side view being from a substantially side perspective, the horizontal mode displays the top view of the aircraft together with a top view of other aircraft near the aircraft, the top view being from a substantially top perspective, and the vertical mode displays the side view of the aircraft together with a side view of other aircraft near the aircraft the side view from a substantially side perspective, and the horizontal mode displays the top view of the aircraft together with a top view of an instrument landing system (ILS) approach including a localizer center beam and a localizer pattern, the top view being from a substantially top perspective, and the vertical mode displays the side view of the aircraft together with a side view of the ILS approach path including a glide slope center beam and a glide slope pattern, the side view being from a substantially side perspective. 12. The system of claim 11, wherein the navigation data module receives global positioning system signals. 13. The system of claim 11, wherein the navigation data module receives data indicating weather including a wind feature. 14. The system of claim 11, wherein the navigation data module receives data from an avionics system of the aircraft. 15. The system of claim 11, wherein the navigation data module receives data from a communications system of the aircraft. 16. The system of claim 11, wherein the navigation data module receives data from a computer readable medium. 17. The system of claim 11, wherein the navigation data module receives data from a network. 18. The system of claim 11, wherein the FAA-defined airspace is one of restricted airspace, class B airspace, class C airspace, and class D airspace. 19. The system of claim 11, further comprising an indication module that provides a voice warning. 20. The system of claim 19, wherein the voice warning is provided in response to one of the FAA-defined airspace, weather, terrain, and other aircraft.
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