Split detent tactile cueing vehicle control system
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IPC분류정보
| 국가/구분 |
United States(US) Patent
등록
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| 국제특허분류(IPC7판) |
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| 출원번호 |
US-0166796
(2002-06-10)
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발명자
/ 주소 |
- Einthoven, Pieter G.
- Miller, David G.
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| 출원인 / 주소 |
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| 대리인 / 주소 |
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| 인용정보 |
피인용 횟수 :
10 인용 특허 :
9 |
초록
▼
A split detent tactile cueing vehicle control system (10) for a vehicle (11) is provided including an active control inceptor system (12). The active system (12) includes a control inceptor (22) having a plurality of positions and a position sensor (42) that generates a control inceptor position sig
A split detent tactile cueing vehicle control system (10) for a vehicle (11) is provided including an active control inceptor system (12). The active system (12) includes a control inceptor (22) having a plurality of positions and a position sensor (42) that generates a control inceptor position signal. The tactile cueing system (10) also includes a plurality of vehicle performance sensors that generate a plurality of vehicle performance signals. A flight controller (20) is electrically coupled to the position sensor (42) and the plurality of vehicle performance sensors, and generates a control inceptor actuation signal by applying a tactile cueing model having a split detent and in response to the position signal and the plurality of vehicle performance signals. A method of performing the same is also provided.
대표청구항
▼
A split detent tactile cueing vehicle control system (10) for a vehicle (11) is provided including an active control inceptor system (12). The active system (12) includes a control inceptor (22) having a plurality of positions and a position sensor (42) that generates a control inceptor position sig
A split detent tactile cueing vehicle control system (10) for a vehicle (11) is provided including an active control inceptor system (12). The active system (12) includes a control inceptor (22) having a plurality of positions and a position sensor (42) that generates a control inceptor position signal. The tactile cueing system (10) also includes a plurality of vehicle performance sensors that generate a plurality of vehicle performance signals. A flight controller (20) is electrically coupled to the position sensor (42) and the plurality of vehicle performance sensors, and generates a control inceptor actuation signal by applying a tactile cueing model having a split detent and in response to the position signal and the plurality of vehicle performance signals. A method of performing the same is also provided. 500, Iwata et al., 369/275.1; US-5602824, 19970200, Ooki et al., 369/275.4; US-5724338, 19980300, Birukawa et al., 369/275.2; US-5764610, 19980600, Yoshida et al., 369/047.2; US-6091682, 20000700, Hikima, 369/047.47; US-6128271, 20001000, Ohta; US-6137756, 20001000, Yoshida et al., 369/053.36; US-6181672, 20010100, Muramatsu et al.; US-6208614, 20010300, Kim, 369/275.4; US-6304535, 20011000, Magome et al., 369/053.2; US-6473377, 20021000, Eguchi et al., 369/053.2; US-6487163, 20021100, Sugaya et al., 369/275.4; US-6507558, 20030100, Aoki, 369/275.3
이 특허에 인용된 특허 (9)
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Walker Laurence A. (Glencoe MO) Stoudt William F. (Florissant MO), Actuator for a g-limiter override.
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Koenig Herbert (Munich DEX), Apparatus for automatically eliminating control force errors in aircraft, especially helicopters.
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Kaye Arthur (Lancashire GB2) Carr Brian (Lancashire GB2) Latham Philip A. (Lancashire GB2), Control apparatus.
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Damotte Sylvain Pascal Frederic,FRX, Device for actuating a controlled member for an aircraft, particularly such as a fly-by-wire helicopter.
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Rollet Philippe Alain Jean,FRX ; Bellera Jacques Serge Louis,FRX, Force-gradient cyclic stick system for a helicopter.
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Gold Phillip J. ; Fogler ; Jr. Donald L., Integrated fire and flight control system for controlling the angle of attack of a rotary wing aircraft.
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Koenig Herbert (Munich DEX), Method and apparatus for stabilizing the steering force in an aircraft, especially a helicopter.
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Gregory William W. (St. Petersburg FL) Kauffman James W. (Palm Harbor FL), Position dependent rate dampening in any active hand controller.
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Gold Phillip J. (Shelton CT) Stiles Lorren (Roxbury CT) Post Joseph A. (Burke VA), Vertical control system for rotary wing aircraft.
이 특허를 인용한 특허 (10)
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Irwin, III, Joseph G.; Einthoven, Pieter G.; Miller, David G.; Spano, Mark S., Active-inceptor tactile-cueing hands-off rate-limit.
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Cherepinsky, Igor, Altitude and acceleration command altitude hold algorithm for rotorcraft with large center of gravity range.
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Kummer, Martin E.; Schlosser, Kevin F.; Gochenour, Daniel V., Clutch pedal control system for an external activation clutch brake.
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Hijikata, Shunsuke; Egami, Masahiro; Kosaka, Norio, Driver assisting system for vehicle and vehicle equipped with the driver assisting system.
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Ishiba, Masatsugu, Flight assistance apparatus.
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Christensen, Kevin Thomas; Shue, Shyhpyng Jack; Caudill, Troy Sheldon, Flight control laws for vertical flight path.
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Jayaraman, Ganga P.; Lyles, Michael L.; Szulyk, Zenon P.; Haack, Bryan R., Force feel using a brushless DC motor.
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Kummer, Martin E.; Schlosser, Kevin F.; Gochenour, Daniel V., Method of controlling an external activation clutch brake.
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Cherepinsky, Igor, Methods and systems for providing constant-feel, multi-axis tactile cues.
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Miller, David George; Gradle, Robert Paul; Taylor, James E., Precision adjust split detent for a vehicle.
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