Abstract:
We consider the 3D problem of controlling the trajectory of an unmanned aerial vehicle (UAV). The purpose of the control is to increase the accuracy of estimating the spatial coordinates of the UAV from discrete angular measurements of the position of a fixed beacon in the process of guidance of the UAV to a given terminal set. The measurements are contaminated by a discrete white noise with known characteristics. The total guidance time is specified.
Keywords:
UAV, angular measurements, control of observations, terminal guidance.
Citation:
D. D. Emel'yanov, E. Ya. Rubinovich, “Trajectory control of 3D observations from an UAV by angular measurements”, Trudy Inst. Mat. i Mekh. UrO RAN, 26, no. 1, 2020, 112–130
\Bibitem{EmeRub20}
\by D.~D.~Emel'yanov, E.~Ya.~Rubinovich
\paper Trajectory control of 3D observations from an UAV by angular measurements
\serial Trudy Inst. Mat. i Mekh. UrO RAN
\yr 2020
\vol 26
\issue 1
\pages 112--130
\mathnet{http://mi.mathnet.ru/timm1703}
\crossref{https://doi.org/10.21538/0134-4889-2020-26-1-112-130}
\elib{https://elibrary.ru/item.asp?id=42492197}
Linking options:
https://www.mathnet.ru/eng/timm1703
https://www.mathnet.ru/eng/timm/v26/i1/p112
This publication is cited in the following 2 articles:
V. S Verba, V. I Merkulov, “Approaches to Optimization of Guidance Methods for High-Speed Intensely Maneuvering Targets. Part 1. Justification of Requirements for Ways of Optimization of Guidance Methods”, Avtomatika i telemehanika, 2024, no. 11, 73
V. S. Verba, V. I. Merkulov, “Approaches to Optimizing Guidance Methods to High-Speed Intensively Maneuvering Targets. Part I. Justifying Requirements for Ways to Optimize Guidance Methods”, Autom Remote Control, 85:11 (2024), 990
Citation in format AMSBIB
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