2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC) 2016
DOI: 10.1109/cgncc.2016.7829064
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Approach to improving maneuver performance of angular rate-based coning algorithms

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Cited by 2 publications
(14 citation statements)
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“…In the SINS attitude updating, the equivalent rotation vector is generally calculated by using the simple approximation form 1,4,79,12,15,17 where φl is the equivalent rotation vector, t is the time, ω is the gyro sensed angular rate vector at the t time, αl is the integral of ω in time domain [tl-1,tl], and δφl is the analytical form of the coning correction.…”
Section: Coning Correction Structure Designmentioning
confidence: 99%
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“…In the SINS attitude updating, the equivalent rotation vector is generally calculated by using the simple approximation form 1,4,79,12,15,17 where φl is the equivalent rotation vector, t is the time, ω is the gyro sensed angular rate vector at the t time, αl is the integral of ω in time domain [tl-1,tl], and δφl is the analytical form of the coning correction.…”
Section: Coning Correction Structure Designmentioning
confidence: 99%
“…In numerical integration algorithm, the integrated angular rate αl is generally achieved by accumulating gyro output, and the numerical coning correction δ^φl 4–8,11,12,15,17 is early approximated using the traditional uncompressed form where Δα s are some angular increment samples spaced adjacently, sequentially, and with a fixed sampling time interval T k , ΔαN-L+1 and ΔαN are, respectively, the first sample and the last sample over time domain [tl-1,tl], ςij is an undetermined correction coefficient, and L and N are, respectively, the number of sample used for calculating αl and δ^φl in a …”
Section: Coning Correction Structure Designmentioning
confidence: 99%
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