Inventor · disambiguated record
Christopher J. Heiberg
Also filed as: HEIBERG CHRISTOPHER J · HEIBERG CHRISTOPHER JAN
15 granted patents·3 pending applications·271 citations·filing 1997–2023
94Inventor score
Top patents by PatentIndex Score
18 records- 0184US6039290ARobust singularity avoidance in satellite attitude controlHONEYWELL INC·Filed 1998·Granted Mar 21, 2000·53 cites·6 claims
- 0282US6131056AContinuous attitude control that avoids CMG array singularitiesHONEYWELL INT INC·Filed 1998·Granted Oct 10, 2000·49 cites·5 claims
- 0380US10543903B2Actuators for high lift devices on aircraftBOEING CO·Filed 2016·Granted Jan 28, 2020·2 cites·21 claims
- 0479US6354163B1Mitigating gimbal induced disturbances in CMG arraysHONEYWELL INT INC·Filed 2000·Granted Mar 12, 2002·26 cites·5 claims
- 0578US10867520B2System and method to modify an aircraft flight trajectoryBOEING CO·Filed 2018·Granted Dec 15, 2020·4 cites·32 claims
- 0677US6415674B1Gear transmission damping apparatus and methodHONEYWELL INT INC·Filed 2000·Granted Jul 9, 2002·18 cites·14 claims
- 0777US6047927AEscaping singularities in a satellite attitude controlHONEYWELL INC·Filed 1998·Granted Apr 11, 2000·38 cites·1 claims
- 0871US7904214B2Singularity escape and avoidance using a virtual array rotationBOEING CO·Filed 2009·Granted Mar 8, 2011·5 cites·6 claims
- 0969US10964220B2Methods and apparatus for providing continuous flight trajectories for aircraftBOEING CO·Filed 2018·Granted Mar 30, 2021·3 cites·20 claims
- 1067US5875676ANon colocated rate sensing for control moment gyroscopesHONEYWELL INC·Filed 1997·Granted Mar 2, 1999·25 cites·14 claims
- 1165US6241194B1Momentum position controlHONEYWELL INT INC·Filed 1999·Granted Jun 5, 2001·26 cites·11 claims
- 1263US7627404B2Singularity escape and avoidance using a virtual array rotationBOEING CO·Filed 2007·Granted Dec 1, 2009·3 cites·7 claims
- 1361US7974746B2Singularity escape and avoidance using a virtual array rotationBOEING CO·Filed 2009·Granted Jul 5, 2011·2 cites·7 claims
- 1453US2024308698A1Systems and methods for combined control moment gyroscope and thruster controlBOEING CO·Filed 2023·Application pending·0 cites
- 1549US2024271695A1Methods and apparatus to passively lubricate a worm gear assemblyBOEING CO·Filed 2023·Application pending·0 cites
- 1647US6772978B2Dynamic unbalance compensation system and methodHONEYWELL INT INC·Filed 2002·Granted Aug 10, 2004·4 cites·25 claims
- 1745US5944761AVariable periodic disturbance rejection filterHONEYWELL INC·Filed 1997·Granted Aug 31, 1999·13 cites·14 claims
- 1840US2013133445A1Control moment gyroscope desaturation in aircraftHEIBERG CHRISTOPHER JAN·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →