이 특허를 인용한 특허 (31)

1. Robins Larry Allen, Adaptive body-bending estimator for use with a missile during flight.

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2. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.

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3. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.

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4. Tran Chuong B. (Lynnwood WA) White Stephen (Bothell WA), Aircraft frequency adaptive modal suppression system.

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5. Tran Chuong B. ; White Stephen, Aircraft frequency adaptive modal suppression system.

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6. Tran Chuong B. ; White Stephen, Aircraft frequency adaptive modal suppression system.

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7. Najmabadi, Kioumars; Tran, Chuong B.; Ho, John Koon-Hung, Aircraft multi-axis modal suppression system.

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8. Najmabadi,Kioumars; Tran,Chuong B.; Ho,John Koon Hung, Aircraft multi-axis modal suppression system.

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9. Kubica, Fran.cedilla.ois, Aircraft with electric flight controls provided with a fuselage able to deform and vibrate.

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10. Charron, Richard, Control system for ornithopter.

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11. Enzinger,Michael; Kordt,Michael, Device and method for damping at least one of a rigid body mode and elastic mode of an aircraft.

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12. Huffman James R. ; Cruickshank Ronald D. ; Jambhekar Shrirang Nikanth ; Collins Russell L., Electronic book and method of capturing and storing a quote therein.

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13. Becker, Juergen, Flight control device for improving the longitudinal stability of an automatically controlled airplane and method of operating same.

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14. Adams, Robert; Schwind, William, Flight control system and method of using piezoelectric modal sensors to mitigate flexible body dynamics.

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15. Kubica,Francois, Inertial reference system for an aircraft.

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16. Nadkarni Arun A. (Kirkland WA) Bryant William F. (Bellevue WA), Method and apparatus for detecting oscillatory phenomena indicative of airflow separation.

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17. Delannoy, Stéphane; Bertin, Thierry, Method and device for piloting an aircraft about a piloting axis.

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18. Krysinski Thomasz,FRX ; Beroul Frederic Andre Henri,FRX, Method and device for reducing the effect of the vibration generated by the driveline of a helicopter.

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19. Krysinsky Tomasz,FRX, Method and device for reducing the vibration generated on the structure of a helicopter.

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20. Huffman James R. ; Jambhekar Shrirang Nikanth, Method and system for encoding a book for reading using an electronic book.

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21. Kubica, Francois, Method for controlling the flight of an aircraft.

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22. Bensch, Lars; Henrichfreise, Hermann; Jusseit, Juergen; Merz, Ludger, Method for reconstructing gusts and structural loads at aircraft, in particular passenger aircraft.

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23. Eglin,Paul, Method for using a steerable tall fin to reduce the vibration generated on the fuselage of a helicopter.

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24. Eglin,Paul, Method for using a tiltable stabilizer to reduce vibration generated on the fuselage of a helicopter.

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25. Huffman James R. ; Cruickshank Ronald D. ; Jambhekar Shrirang Nikanth ; Collins Russell L., Method of substituting names in an electronic book.

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26. Chakravarty, Abhijit J. M.; Hamley, James P.; Romanosky, Joseph M., Methods and systems for air vehicle telemetry.

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27. Emilio A. Fernandez, Microprocessor based simulated book.

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28. Kubica,Fran챌ois; Briere,Dominique, Process for countering the vibrations induced in an aircraft by the windmilling of a fan and system of electric flight controls implementing this process.

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29. Juergen Becker DE, System and method for compensating structural vibrations of an aircraft caused by outside disturbances.

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30. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E., Yaw damping system and method for aircraft.

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31. Hagerott, Steven G.; Klausmeyer, Steven; Mendoza, Gonzalo E., Yaw damping system and method for aircraft.

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