Decision aid device for assisting the landing of an aircraft on the deck of a ship
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G06F-019/00
G06G-007/70
출원번호
US-0945602
(2010-11-12)
등록번호
US-8612070
(2013-12-17)
우선권정보
FR-09 05470 (2009-11-13)
발명자
/ 주소
Geoffroy, Rémi
Garrec, Patrick
Thiry, Yannick
Cazaux, Patrick
출원인 / 주소
Thales
대리인 / 주소
Baker & Hostetler LLP
인용정보
피인용 횟수 :
5인용 특허 :
5
초록▼
A device for aiding the deck-landing of an aircraft, the aircraft being controlled remotely from a mobile station, such as a ship, includes means for receiving data from the aircraft, notably attitudes of the aircraft, the aircraft hovering ready to land on deck, the deck-landing decision having to
A device for aiding the deck-landing of an aircraft, the aircraft being controlled remotely from a mobile station, such as a ship, includes means for receiving data from the aircraft, notably attitudes of the aircraft, the aircraft hovering ready to land on deck, the deck-landing decision having to be taken under certain conditions that must all be met, the device including a computer making it possible to deliver temporal indicators indicating that all the conditions are met. The device includes a temporal gauge including a temporal graduation indicating mobile graphical zones representing the periods during which all the conditions are met for authorizing a deck-landing.
대표청구항▼
1. A device for aiding the deck-landing of a pilotless rotary-wing aircraft on a mobile station, called a ship, the aircraft being intended to be controlled remotely on the basis of said device, comprising: means for receiving data from the aircraft, comprising attitudes of the aircraft and a comput
1. A device for aiding the deck-landing of a pilotless rotary-wing aircraft on a mobile station, called a ship, the aircraft being intended to be controlled remotely on the basis of said device, comprising: means for receiving data from the aircraft, comprising attitudes of the aircraft and a computer, the aircraft hovering ready to land on deck, the deck-landing decision having to be made under certain conditions comprising a first set of predictive criteria and a second set of non-predictive criteria, the predictive criteria corresponding to parameters measured by the computer and whose value may be extrapolated in the near future, the predictive criteria relating to the attitudes of the aircraft and of the ship, amplitude and speed of the swell, a strength and direction of wind on the deck of the ship, the non-predictive criteria corresponding to parameters not measurable by the computer, the non-predictive criteria relating to the clearance of the deck,wherein the computer makes it possible to deliver at least one temporal indicator indicating that the predictive criteria are favourable or unfavourable to a deck-landing, and a display making it possible to represent the indicator in a first state when the predictive criteria are favourable to deck-landing. 2. A device for aiding the deck-landing of an aircraft according to claim 1, wherein the device further comprises acknowledgement means allowing an operator to acknowledge the non-predictive criteria, the temporal indicator generated previously by the computer being represented in a second state when the operator acknowledges the non-predictive criteria. 3. A device for aiding the deck-landing of an aircraft according to claim 1, wherein the temporal indicator comprises at least one window scrolling over a time-graduated gauge. 4. A device for aiding the deck-landing of an aircraft according to claim 3, wherein a time limit is defined in such a way that a window sliding beyond this time limit and for which the window's remaining time no longer allows the deck-landing of the aircraft, no longer allows the operator to acknowledge the non-predictive criteria for this window. 5. A device for aiding the deck-landing of an aircraft according to claim 4, wherein the temporal indicator is represented in a third state when the window oversteps the time limit whilst the operator has acknowledged the non-predictive criteria. 6. A device for aiding the deck-landing of an aircraft according to claim 4, wherein the temporal indicator is represented in a fourth state when the window oversteps the time limit whilst the operator has not acknowledged the non-predictive criteria. 7. A device for aiding the deck-landing of an aircraft according to claim 1, wherein the predictive criteria comprise a value corresponding to the exceeding of at least one authorized maximum deviation of an attitude of the ship. 8. A device for aiding the deck-landing of an aircraft according to claim 1, wherein the predictive criteria comprise a value corresponding to exceeding at least one authorized maximum deviation of an attitude of the aircraft. 9. A device for aiding the deck-landing of an aircraft according to claim 1, wherein the predictive criteria comprise a value corresponding to exceeding an authorized maximum deviation of the amplitude of the swell. 10. A device for aiding the deck-landing of an aircraft according to claim 1, wherein the predictive criteria comprise a value corresponding to exceeding an authorized maximum deviation of the strength of the wind at deck level. 11. A device for aiding the deck-landing of an aircraft according to claim 1, wherein the predictive criteria comprise a value corresponding to the direction of the wind at deck level. 12. A device for aiding the deck-landing of an aircraft according to claim 1, wherein the non-predictive criteria comprise the finding that a zone of the deck is clear. 13. A device for aiding the deck-landing for an aircraft according to claim 1, wherein the aircraft comprises means for receiving the data generated by the computer of the ship and display means making it possible to display the temporal indicator. 14. A device for aiding the deck-landing of a pilotless rotary-wing aircraft on a mobile station, called a ship, the aircraft being intended to be controlled remotely on the basis of said device, comprising: a computer configured to obtain attitudes of the aircraft, the aircraft hovering ready to land on deck, the deck-landing decision having to be made under certain conditions comprising a first set of predictive criteria and a second set of non-predictive criteria, the predictive criteria corresponding to parameters measured by the computer and whose value may be extrapolated in the near future, the predictive criteria relating to the attitudes of the aircraft and of the ship, amplitude and speed of swell, a strength and direction of wind on the deck of the ship, the non-predictive criteria corresponding to parameters not measurable by the computer, the non-predictive criteria relating to the clearance of the deck,wherein the computer makes it possible to deliver at least one temporal indicator indicating that the predictive criteria are favourable or unfavourable to a deck-landing, and a display making it possible to represent the indicator in a first state when the predictive criteria are favourable to deck-landing. 15. The device for aiding the deck-landing of an aircraft according to claim 14, wherein the device is further configured to allow an operator to acknowledge the non-predictive criteria, the temporal indicator generated previously by the computer being represented in a second state when the operator acknowledges the non-predictive criteria. 16. A device for aiding a deck-landing of a pilotless rotary-wing aircraft on a ship, the aircraft being controlled remotely on a basis of the device, comprising: a computer configured to obtain attitudes of the aircraft, the aircraft hovering ready to land on deck, a deck-landing decision being made under certain conditions comprising a first set of predictive criteria and a second set of non-predictive criteria, the predictive criteria corresponding to parameters measured by the computer and whose value may be extrapolated in the near future, the predictive criteria relating to the attitudes of the aircraft and of the ship, amplitude and speed of swell, a strength and direction of wind on the deck of the ship, the non-predictive criteria corresponding to parameters not measurable by the computer, the non-predictive criteria relating to the clearance of the deck;the computer being configured to deliver at least one temporal indicator indicating that the predictive criteria are favourable or unfavourable to a deck-landing; anda display configured to represent the indicator in a first state when the predictive criteria are favourable to deck-landing. 17. The device for aiding the deck-landing of an aircraft according to claim 16, wherein the device is further configured to allow an operator to acknowledge the non-predictive criteria, the temporal indicator generated previously by the computer being represented in a second state when the operator acknowledges the non-predictive criteria.
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이 특허에 인용된 특허 (5)
Suddreth, John G.; Gannon, Aaron J.; He, Gang; Feyereisen, Thea L., Aircraft display systems and methods for enhanced display of landing information.
Moravek, Zdenek; Sosovicka, Robert; Magula, Filip; Kunes, David; Sprinarova, Katerina, Methods and systems facilitating holding for an unavailable destination.
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