Stability analysis of gyroscopic systems with integral correction.
- Published in:
- International Applied Mechanics, 2009, v. 45, n. 11, p. 1248, doi. 10.1007/s10778-010-0266-8
- By:
- Publication type:
- Article
Works matching DE "ARTIFICIAL horizons (Aeronautical instruments)"
Results: 6
1
2
Attitude Indicator Design in Primary Flight Display: Revisiting an Old Issue With Current Technology.
- Published in:
- International Journal of Aerospace Psychology, 2018, v. 28, n. 1/2, p. 46, doi. 10.1080/24721840.2018.1486714
- By:
- Publication type:
- Article
3
Six-position calibration for the fiber optic gyro based on a double calculating program.
- Published in:
- Optical Engineering, 2013, v. 52, n. 4, p. 1, doi. 10.1117/1.OE.52.4.043603
- By:
- Publication type:
- Article
4
DYNAMIC CHARACTERISTICS OF MECHANICAL VIBRATION GYROSCOPES AS SENSORS OF NAVIGATION SYSTEMS.
- Published in:
- Naukovi visti NTUU - KPI, 2006, v. 2006, n. 6, p. 90
- By:
- Publication type:
- Article
5
Performance Testing of a Magnetically Suspended Double Gimbal Control Moment Gyro Based on the Single Axis Air Bearing Table.
- Published in:
- Sensors (14248220), 2012, v. 12, n. 7, p. 9129, doi. 10.3390/s120709129
- By:
- Publication type:
- Article
6
Optimal Design of a Center Support Quadruple Mass Gyroscope (CSQMG).
- Published in:
- Sensors (14248220), 2016, v. 16, n. 5, p. 613, doi. 10.3390/s16050613
- By:
- Publication type:
- Article