2014
DOI: 10.1061/(asce)as.1943-5525.0000284
|View full text |Cite
|
Sign up to set email alerts
|

Position Estimation for Projectiles Using Low-Cost Sensors and Flight Dynamics

Abstract: Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing the burden, to Department of Defense, Washington Headquarters Services, Directorate for Informat… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2018
2018
2022
2022

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 8 publications
(2 citation statements)
references
References 29 publications
0
2
0
Order By: Relevance
“…The instant when the shell reaches Mach 1 is easily detected on the longitudinal accelerometer, under the form of a sudden jump of the signal. Comparing the value of 317 8 m/s obtained from the frequency estimate through the velocity model with Mach 1 (332 m/s) 11 , we deduce that our velocity estimate is biased (at this particular instant) by ≈ 13 2 m/s. Applying the inverse of the velocity model, we deduce our frequency estimate is biased by ≈ 2 Hz, and decide to apply a constant bias correction over the whole time interval.…”
Section: Reference Velocitymentioning
confidence: 63%
See 1 more Smart Citation
“…The instant when the shell reaches Mach 1 is easily detected on the longitudinal accelerometer, under the form of a sudden jump of the signal. Comparing the value of 317 8 m/s obtained from the frequency estimate through the velocity model with Mach 1 (332 m/s) 11 , we deduce that our velocity estimate is biased (at this particular instant) by ≈ 13 2 m/s. Applying the inverse of the velocity model, we deduce our frequency estimate is biased by ≈ 2 Hz, and decide to apply a constant bias correction over the whole time interval.…”
Section: Reference Velocitymentioning
confidence: 63%
“…Another natural follow-up is to use these results to improve the estimation of the projectile's attitude and position [11][27] [8]…”
Section: Conclusion and Associated Workmentioning
confidence: 99%