نتایج جستجو برای: rate gyro

تعداد نتایج: 961439  

2001
Hakyoung Chung Lauro Ojeda Johann Borenstein

Recently, fiber optic gyros with very low drift rates have become available and affordable. Because of their low drift rate attention is warranted to sources of errors that were previously considered as of secondary importance. In the KVH E-Core RD2100 gyros, we found that the temperature dependency and the non-linearity of the scale-factor caused significant errors. A precision calibration pro...

1999
Stergios I. Roumeliotis Gaurav S. Sukhatme George A. Bekey

The mobile robot localization problem is treated as a two-stage iterative estimation process. The attitude is estimated rst and is then available for position estimation. The indirect (error state) form of the Kalman lter is developed for attitude estimation when applying gyro modeling. The main bene t of this choice is that complex dynamic modeling of the mobile robot and its interaction with ...

2003
Dongwon Jung Panagiotis Tsiotras

This article presents the details of a newly constructed 3-dof experimental spacecraft simulator facility at the School of Aerospace Engineering at the Georgia Institute of Technology. The main component of the facility is a cylindrical platform located on a hemi-spherical air bearing that allows friction-free rotation about three axes. The facility includes a variety of actuators and sensors: ...

2002
T. L. Rhodes J.-N. Leboeuf D. W. Ross J. Candy G. R. McKee R. V. Bravenec E. J. Doyle R. J. Groebner W. A. Peebles R. D. Sydora L. Zeng G. Wang

Experimental turbulence and transport characteristics in DIII–D plasmas have been compared with similar quantities calculated from gyro-kinetic and gyro-fluid turbulence simulations. Turbulent radial correlation lengths ∆r from DIII–D L–mode plasmas scale as 5 to 10 ρs (ρs = ion gyro-radius evaluated using the electron temperature) and are independent of the poloidal magnetic field. Comparisons...

2013
S. Naveen Siva Rama Krishna M. K. Gupta

In air crafts, missiles and ships, during their motion, the sensors are prone to undergo lot of vibrations and shocks. Because of their sensitivity to these environments they malfunction. In order to avoid this situation all the sensors are modelled and analysed at the ground for different parameters viz. temperature, vibration and shock etc. A Ring Laser Gyro (RLG) is used for sensing the angl...

2005
M. J. Kosch T. Pedersen

High-power high-frequency radio waves beamed into the ionosphere cause plasma turbulence, which can accelerate electrons. These electrons collide with the F-layer neutral oxygen causing artificial optical emissions identical to natural aurora. Pumping at electron gyro-harmonic frequencies has special significance as many phenomena change their character. In particular, artificial optical emissi...

2008
Edward Boje

This paper examines the estimation of the state of an object moving in the horizontal plane using two, two-axis accelerometers and no rate gyro. Second order approximations are developed for estimating the state noise covariance in the inertial reference frame from the known measurement covariance of the sensors. These approximations can be integrated with position and heading measurements into...

2014
Xing Fei Chen Nan You Zheng Sun Ting Mohammad Younis

The traditional approach of star tracker for determining the centroid of spot requires enough energy and good shape, so a relatively long exposure time and stable three-axis state become necessary conditions to maintain high accuracy, these limit its update rate and dynamic performance. In view of these issues, this paper presents an approach for determining the centroid of star spot which base...

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