Aircraft systems and methods for attitude recovery
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G08B-023/00
B64D-045/00
G01C-023/00
출원번호
US-0901022
(2013-05-23)
등록번호
US-9221552
(2015-12-29)
발명자
/ 주소
Conner, Kevin J
Ishihara, Yasuo
Feyereisen, Thea L.
Morgan, John Allan
출원인 / 주소
HONEYWELL INTERNATIONAL INC.
대리인 / 주소
Ingrassia Fisher & Lorenz, P.C.
인용정보
피인용 횟수 :
4인용 특허 :
15
초록▼
A vehicle system is provided. The system includes a processor configured to receive data representative of a current attitude and a desired attitude and to generate display signals associated with the current attitude and the desired attitude. The system further includes a display device configured
A vehicle system is provided. The system includes a processor configured to receive data representative of a current attitude and a desired attitude and to generate display signals associated with the current attitude and the desired attitude. The system further includes a display device configured to receive the display signals and operable to selectively render an image including roll angle alert symbology. The roll angle alert symbology includes a first curved arrow.
대표청구항▼
1. A vehicle system comprising: a processor configured to receive data representative of a current attitude and a desired attitude and to generate display signals associated with the current attitude and the desired attitude, wherein the processor is configured to compare the current altitude to the
1. A vehicle system comprising: a processor configured to receive data representative of a current attitude and a desired attitude and to generate display signals associated with the current attitude and the desired attitude, wherein the processor is configured to compare the current altitude to the desired altitude to determine a roll angle, the processor further configured to establish a roll angle alert when the roll angle exceeds a predetermined roll angle; anda display device configured to receive the display signals and operable to selectively render an image including roll angle alert symbology, the roll angle alert symbology including a first curved arrow, wherein the display device is configured to only display the roll angle alert symbology during the roll angle alert. 2. The vehicle system of claim 1, wherein the processor is configured to determine a roll angle correction direction, and wherein the first curved arrow is oriented in the roll angle correction direction. 3. The vehicle system of claim 1, wherein the first curved arrow is dynamically rendered to change appearance. 4. The vehicle system of claim 1, wherein the first curved arrow has a length of at least 30°. 5. The vehicle system of claim 1, wherein the first curved arrow has a length of at least 45°. 6. The vehicle system of claim 1, wherein the first curved arrow is dynamically rendered to grow in length over time. 7. The vehicle system of claim 1, wherein the first curved arrow grows from an initial length of between approximately 30° and approximately 45° to a final length of between approximately 90° to approximately 180°. 8. The vehicle system of claim 1, wherein the first curved arrow grows from an initial length to a final length at approximately a roll angle pointer. 9. A vehicle system comprising: a processor configured to receive data representative of a current attitude and a desired attitude and to generate display signals associated with the current attitude and the desired attitude; anda display device configured to receive the display signals and operable to selectively render an image including roll angle alert symbology, the roll angle alert symbology including a first curved arrow,wherein the image further includes wing symbology, and wherein the first curved arrow has a base at the wing symbology. 10. The vehicle system of claim 9, wherein the roll angle alert symbology further includes a second curved arrow, and wherein the first curved arrow is selectively positioned above the wing symbology and the second curved arrow is selectively positioned below the wing symbology. 11. The vehicle system of claim 10, wherein the current attitude includes a current pitch of the aircraft, and wherein the display device is configured to selectively render at least one of the first curved arrow and the second curved arrow based on the current pitch of the vehicle. 12. The vehicle system of claim 11, wherein, when the current pitch indicates a neutral pitch condition, the display device is configured to simultaneously display the first curved arrow and the second curved arrow, wherein, when the current pitch indicates a nose down pitch condition, the display device is configured to display only the first curved arrow, andwherein, when the current pitch indicates a nose up pitch condition, the display device is configured to display only the second curved arrow. 13. A vehicle display method, comprising the steps of: receiving data representative of a current attitude and a desired attitude for a vehicle;evaluating a roll alert condition of the vehicle;displaying, during the roll alert condition, a first curved arrow on an attitude indicator; andmodifying, during the roll alert condition, an appearance of the first curved arrow, wherein the displaying step further includes displaying, during the roll alert condition, a second curved arrow on the attitude indicator. 14. The method of claim 13, further comprising the step of determining a roll angle correction direction; and wherein the displaying step includes orienting the first curved arrow in the roll angle correction direction. 15. The method of claim 13, wherein the modifying step includes dynamically rendering the first curved arrow to change appearance, and wherein the displaying step includes displaying the first curved arrow with a length of at least 30°. 16. The method of claim 13, wherein the image further includes wing symbology, and wherein the displaying step includes displaying a base of the first curved arrow at the wing symbology. 17. The method of claim 13, wherein the displaying step includes displaying the first curved arrow selectively positioned above the wing symbology and displaying the second curved arrow selectively positioned below the wing symbology. 18. The method of claim 17, further comprising the step of evaluating a current pitch, and wherein the displaying step includes,when the current pitch indicates a neutral pitch condition, simultaneously displaying the first curved arrow and the second curved arrow,when the current pitch indicates a nose down pitch condition, displaying only the first curved arrow, andwhen the current pitch indicates a nose up pitch condition, displaying only the second curved arrow.
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이 특허에 인용된 특허 (15)
Stanis John W. (3020 NE. 13th Ave. Pompano Beach FL 33069), Aircraft banking angle indicator.
Shiozaki, Tomoyuki, Imaging apparatus including a control unit configured to change a correction value for correcting an output of an orientation detection unit.
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