This citation summarizes a one-page announcement of technology available for utilization. A microprocessor-controlled inertial navigation system is based upon a pendulous two-axis gimbal assembly. It is considerably simpler and less costly than conventional platform or strap-down inertial guidance and is therefore especially appropriate for small aircraft. ...FOR ADDITIONAL INFORMATION: Contact: Ames Research Center Mail Code: 200-11A Moffett Field, CA 94035. Refer to ARC-11257/DB.
Less-Costly Inertial Guidance: Pendulum-based system uses only two gyros and no accelerometers
1982
1 pages
Report
Keine Angabe
Englisch
NTRS | 1982
|Shock tests of gyros and accelerometers
AIAA | 1979
|Micromechanical Gyros & Accelerometers for Digital Navigation & Control
Online Contents | 2009
|MEMS Low Cost Inertial Grade Accelerometers and Gyros Using a Common, Bulk Micromachining Process
British Library Conference Proceedings | 1999
|