IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0135995
(2002-04-30)
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발명자
/ 주소 |
- Silder, Jr., Stephen H.
- Evans, Charles W.
- Thornberg, Christopher A.
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출원인 / 주소 |
- Sikorsky Aircraft Corporation
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대리인 / 주소 |
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인용정보 |
피인용 횟수 :
13 인용 특허 :
3 |
초록
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A method for automating a landing maneuver for an aircraft, comprising the steps of generating an approach profile comprising an initial approach fix (IAF), a flight path, a landing decision point, a balked landing route, a pre-landing point, and a landing point, engaging an automated approach syste
A method for automating a landing maneuver for an aircraft, comprising the steps of generating an approach profile comprising an initial approach fix (IAF), a flight path, a landing decision point, a balked landing route, a pre-landing point, and a landing point, engaging an automated approach system to access the approach profile, receiving periodic position data of the aircraft, comparing the position data to the approach profile to compute a plurality of deviations each time the position data is received, outputting the plurality of deviations to a display, converting the plurality of deviations into a plurality of control commands, and maneuvering the aircraft in response to the control commands along the flight path.
대표청구항
▼
A method for automating a landing maneuver for an aircraft, comprising the steps of generating an approach profile comprising an initial approach fix (IAF), a flight path, a landing decision point, a balked landing route, a pre-landing point, and a landing point, engaging an automated approach syste
A method for automating a landing maneuver for an aircraft, comprising the steps of generating an approach profile comprising an initial approach fix (IAF), a flight path, a landing decision point, a balked landing route, a pre-landing point, and a landing point, engaging an automated approach system to access the approach profile, receiving periodic position data of the aircraft, comparing the position data to the approach profile to compute a plurality of deviations each time the position data is received, outputting the plurality of deviations to a display, converting the plurality of deviations into a plurality of control commands, and maneuvering the aircraft in response to the control commands along the flight path. ngs IEEE Nucl. Sci. Symp. 1988, 5 pages. Irving Weinberg, Stan Majewski, Andrew Weisenberger, Allen Markowitz, Luigi Aloj, Lukasz Majewski, David Danforth, James Mulshine, Kenneth Cowan, JoAnne Zujewski, Catherine Chow, Elizabeth Jones, Victoria Chang, Wendie Berg and Joseph Frank, Preliminary Results for Positron Emission Mammography: Real-time Funcation Breast Imaging in a Conventional Mammography Gantry, European Journal of Nuclear Medicine, vol. 23, No. 7, Jul. 1996. C.J. Thompson, K. Murthy, I.N. Weinberg, F. Mako, Feasibility Study for Positron Emission Mammography, Medical Physics, vol. 21, No. 4, Apr. 1994, p. 529-538. Martin Hanke, Andreas Neubauer, Otmar Scherzer, A Convergence Analysis of the Landweber Iteration for Nonlinear III-posed Problems, Numer. Math. 72:21-37 (1995). Donald W. Wilson and Benjamin M. W. Tsui, Noise Properties of Filtered-Backprojection and ML-EM Reconstructed Emission Tomographic Images, IEEE Transactions on Nuclear Science, vol. 40, No. 4, Aug. 1993, pp. 1198-12
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