Inventor · disambiguated record
Michael Surauer
Also filed as: SURAUER MICHAEL · SURAUER MICHAEL ALOIS
17 granted patents·447 citations·filing 1981–2016
95Inventor score
Files withDAIMLER BENZ AEROSPACE AG5DEUTSCHE AEROSPACE5MESSERSCHMITT BOELKOW BLOHM5DIAMLER BENZ AEROSPACE AG1MBDA DEUTSCHLAND GMBH1
Top patents by PatentIndex Score
17 records- 0187US4567564AArrangement for the attitude stabilization of flexible vehicles with weakly-dampened structural vibrations and discontinuous control interventionMESSERSCHMITT BOELKOW BLOHM·Filed 1981·Granted Jan 28, 1986·49 cites·19 claims
- 0284US5931421AArrangement for attitude control and stabilization of a three axes stabilized spacecraftDAIMLER BENZ AEROSPACE AG·Filed 1996·Granted Aug 3, 1999·69 cites·4 claims
- 0382US5697582AMethod of adjusting the position of satellites by means of solar pressure torquesDEUTSCHE AEROSPACE·Filed 1992·Granted Dec 16, 1997·52 cites·13 claims
- 0481US5042752AApparatus for controlling the attitude of and stabilizing an elastic bodyMESSERSCHMITT BOELKOW BLOHM·Filed 1988·Granted Aug 27, 1991·53 cites·22 claims
- 0573US5957410AEarth oriented satellite and process for controlling the position, nutation and spinDAIMLER BENZ AEROSPACE AG·Filed 1996·Granted Sep 28, 1999·36 cites·3 claims
- 0671US5996941AMethod for controlling the attitude of a three-axis stabilized, earth oriented bias momentum spacecraftDAIMLER BENZ AEROSPACE AG·Filed 1997·Granted Dec 7, 1999·35 cites·3 claims
- 0768US4954732AAdaptive nonlinear frequency domain filter with low phase lossMESSERSCHMITT BOELKOW BLOHM·Filed 1988·Granted Sep 4, 1990·17 cites·25 claims
- 0863US4914564AAdaptive control system of high accuracy and low corrective energy consumptionMESSERSCHMITT BOELKOW BLOHM·Filed 1987·Granted Apr 3, 1990·22 cites·16 claims
- 0961US5984238AMethod and system for the autonomous on-board determination of the position of a satelliteDIAMLER BENZ AEROSPACE AG·Filed 1998·Granted Nov 16, 1999·30 cites·4 claims
- 1061US4505206AMethod and circuit arrangement for optimally controlling an air gap between an electromagnetically levitated vehicle and a railMESSERSCHMITT BOELKOW BLOHM·Filed 1982·Granted Mar 19, 1985·18 cites·2 claims
- 1156US5433402AAttitude control process and device for a spacecraft to be rotated around an axis of a bodyDEUTSCHE AEROSPACE·Filed 1992·Granted Jul 18, 1995·24 cites·15 claims
- 1245US5558305AMeasuring arrangement useful for controlling the attitude of a three-axis stabilized satellite, corresponding evaluation process, regulating system and processDEUTSCHE AEROSPACE·Filed 1992·Granted Sep 24, 1996·12 cites·9 claims
- 1343US5535965AThree-axis stabilized, earth-oriented satellite and a corresponding sun and earth acquisition processDEUTSCHE AEROSPACE·Filed 1992·Granted Jul 16, 1996·11 cites·20 claims
- 1442US5597143AProcess and a device for controlling the attitude of a three-axis stabilized spinning spacecraftDEUTSCHE AEROSPACE·Filed 1993·Granted Jan 28, 1997·12 cites·4 claims
- 1530US5906338ASun search method and apparatus for a satellite stabilized in three axesDAIMLER BENZ AEROSPACE AG·Filed 1996·Granted May 25, 1999·4 cites·13 claims
- 1628US5934619ASatellite positioning apparatus and processDAIMLER BENZ AEROSPACE AG·Filed 1996·Granted Aug 10, 1999·3 cites·7 claims
- 1725US9874422B2Stationary and mobile test device for missilesMBDA DEUTSCHLAND GMBH·Filed 2016·Granted Jan 23, 2018·0 cites·6 claims
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