DocumentCode
1945710
Title
Modified strapdown inertial navigator error models
Author
Scherzinger, Bruno M. ; Reid, D. Blake
Author_Institution
Appl. Anal. Corp., Markham, Ont., Canada
fYear
1994
fDate
11-15 Apr 1994
Firstpage
426
Lastpage
430
Abstract
The paper revisits the problem of error modeling for strapdown INS for the purpose of navigation sensor blending with a Kalman filter. This problem has been addressed repeatedly over the last 30 years, and different perspectives on INS error modeling have emerged. The paper reviews these, focussing in particular on the properties and relative advantages and disadvantages of the φ-angle and ψ-angle error models. The paper then addresses some new concepts for the design of a Kalman filter model for integrated navigation. The sometimes troublesome problem of the explicit occurrence of the specific force in both error models is averted with the modified φ-angle and ψ-angle error models proposed in the paper, in which the explicit representation of the specific force is canceled via a transformation of the velocity error states
Keywords
Kalman filters; aircraft; error analysis; filtering and prediction theory; inertial navigation; φ-angle error models; ψ-angle error models; INS; Kalman filter; design; modified strapdown inertial navigator error models; navigation sensor blending; specific force; velocity error states; Acceleration; Accelerometers; Analytical models; Bandwidth; Computer errors; Earth; Error correction; Inertial navigation; State estimation; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Position Location and Navigation Symposium, 1994., IEEE
Conference_Location
Las Vegas, NV
Print_ISBN
0-7803-1435-2
Type
conf
DOI
10.1109/PLANS.1994.303345
Filename
303345
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