DocumentCode
2636135
Title
Milli-HRG inertial sensor assembly ??? a reality
Author
Rozelle, D.M. ; Meyer, A.D. ; Trusov, A.A. ; Sakaida, D.K.
Author_Institution
Adv. Navig. Syst., Northrop Grumman Syst. Corp., Woodland Hills, CA, USA
fYear
2015
fDate
23-26 March 2015
Firstpage
1
Lastpage
4
Abstract
The Hemispherical Resonator Gyro (HRG) has proven itself to be an ultra-reliable technology for space application with over 30 million operation hours and 100% mission success. Northrop Grumman Advanced Navigation Systems is developing a small size and lightweight terrestrial inertial sensor assembly (ISA) based on the HRG approach. This ISA will be the core of future inertial measurement unit (IMU) and inertial navigation system (INS) product lines.
Keywords
calibration; gyroscopes; inertial navigation; inertial systems; Northrop Grumman Advanced Navigation Systems; hemispherical resonator gyro; inertial measurement unit; inertial navigation system; lightweight terrestrial inertial sensor assembly; milliHRG inertial sensor assembly; Accuracy; Calibration; Electrodes; Flexible printed circuits; Real-time systems; Stability analysis; Thermal stability; CVG; HRG; Hemispherical Resonator Gyro; ISA; Self-Calibration;
fLanguage
English
Publisher
ieee
Conference_Titel
Inertial Sensors and Systems (ISISS), 2015 IEEE International Symposium on
Conference_Location
Hapuna Beach, HI
Type
conf
DOI
10.1109/ISISS.2015.7102386
Filename
7102386
Link To Document