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VALORBEC SOCIETE EN COMMANDITE
| VALORBEC SOCIETE EN COMMANDITE Patent applications | ||
| Patent application number | Title | Published |
|---|---|---|
| 20120121167 | FINITE DATASET INTERPOLATION METHOD - The invention provides a fast method for a high-quality interpolation of a finite multidimensional dataset. It has particular application in digital image processing, including, but not limited to, processing of both still images and real-time image/data processing. The method uses discrete cosine and sine transforms of appropriate types to covert, in blocks of desired size, the initial dataset to the frequency domain. Proposed interpolators calculate a chain of inverse transforms of non-square sizes that perform the interpolation. The larger transform is broken into smaller transforms of non-square size using a recursive size reduction process of FFT-type, and the smaller transforms are calculated directly exploiting the symmetry properties of smaller interpolator functions involved. An output dataset is then assembled using the calculated transforms. The method avoids computationally costly process of inflating the coefficient space by padding zeros exploited for DCT-based interpolations previously. | 05-17-2012 |
| 20110231037 | HARD-LANDING OCCURRENCE DETERMINATION SYSTEM AND METHOD FOR AIRCRAFT - A method for determining a hard-landing occurrence for an aircraft has sensors at selected positions of the aircraft. A model defining critical points throughout the aircraft is obtained. Data is received from the sensors when the aircraft lands. Diagnosis values for all critical points of the aircraft are calculated by applying the model to the data from the sensors. The diagnosis values are compared to threshold values for the critical points of the aircraft. A hard-landing occurrence is determined from the comparison between the diagnosis value and the threshold value. A hard-landing occurrence determination system for an aircraft is also provided. Sensors at selected positions of the aircraft provide data related to accelerations at landing of the aircraft. A diagnosis processor unit determines the hard-landing occurrence, and comprises a model database, a threshold database and a threshold comparator. A hard-landing occurrence interface signals a hard-landing occurrence. | 09-22-2011 |