Moving observer trajectory control by angular measurements in tracking problem
Abstract An optimal path synthesis problem for a moving observer that performs angular observations over a target moving uniformly along a straight line on a plane is solved. It is supposed that elevation and azimuth angles can be observed when the observer moves in space and only the azimuth angle...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Andreev, K. V. [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2016 |
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| Schlagwörter: |
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| Anmerkung: |
© Pleiades Publishing, Ltd. 2016 |
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| Übergeordnetes Werk: |
Enthalten in: Automation and remote control - Pleiades Publishing, 1957, 77(2016), 1 vom: Jan., Seite 106-129 |
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| Übergeordnetes Werk: |
volume:77 ; year:2016 ; number:1 ; month:01 ; pages:106-129 |
| Links: |
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| DOI / URN: |
10.1134/S0005117916010069 |
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OLC2060908876 |
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| 520 | |a Abstract An optimal path synthesis problem for a moving observer that performs angular observations over a target moving uniformly along a straight line on a plane is solved. It is supposed that elevation and azimuth angles can be observed when the observer moves in space and only the azimuth angle can be observed when the observer moves on a plane. Observer’s trajectories are obtained with the help of Pontryagin’smaximum principle as numerical solutions of an optimal control problem. As a performance criterion the trace of covariance matrix of the target motion elements estimate is used. A possibility of solving the problem in real time on board for unmanned aerial vehicle is investigated. A comparison with the scenario of two unmanned aerial vehicles using is given. | ||
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10.1134/S0005117916010069 doi (DE-627)OLC2060908876 (DE-He213)S0005117916010069-p DE-627 ger DE-627 rakwb eng 000 620 VZ Andreev, K. V. verfasserin aut Moving observer trajectory control by angular measurements in tracking problem 2016 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2016 Abstract An optimal path synthesis problem for a moving observer that performs angular observations over a target moving uniformly along a straight line on a plane is solved. It is supposed that elevation and azimuth angles can be observed when the observer moves in space and only the azimuth angle can be observed when the observer moves on a plane. Observer’s trajectories are obtained with the help of Pontryagin’smaximum principle as numerical solutions of an optimal control problem. As a performance criterion the trace of covariance matrix of the target motion elements estimate is used. A possibility of solving the problem in real time on board for unmanned aerial vehicle is investigated. A comparison with the scenario of two unmanned aerial vehicles using is given. Remote Control Optimal Control Problem Pitch Angle Unmanned Aerial Vehicle Elevation Angle Rubinovich, E. Ya. aut Enthalten in Automation and remote control Pleiades Publishing, 1957 77(2016), 1 vom: Jan., Seite 106-129 (DE-627)129603481 (DE-600)241725-X (DE-576)015097315 0005-1179 nnns volume:77 year:2016 number:1 month:01 pages:106-129 https://doi.org/10.1134/S0005117916010069 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-MAT GBV_ILN_70 AR 77 2016 1 01 106-129 |
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10.1134/S0005117916010069 doi (DE-627)OLC2060908876 (DE-He213)S0005117916010069-p DE-627 ger DE-627 rakwb eng 000 620 VZ Andreev, K. V. verfasserin aut Moving observer trajectory control by angular measurements in tracking problem 2016 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2016 Abstract An optimal path synthesis problem for a moving observer that performs angular observations over a target moving uniformly along a straight line on a plane is solved. It is supposed that elevation and azimuth angles can be observed when the observer moves in space and only the azimuth angle can be observed when the observer moves on a plane. Observer’s trajectories are obtained with the help of Pontryagin’smaximum principle as numerical solutions of an optimal control problem. As a performance criterion the trace of covariance matrix of the target motion elements estimate is used. A possibility of solving the problem in real time on board for unmanned aerial vehicle is investigated. A comparison with the scenario of two unmanned aerial vehicles using is given. Remote Control Optimal Control Problem Pitch Angle Unmanned Aerial Vehicle Elevation Angle Rubinovich, E. Ya. aut Enthalten in Automation and remote control Pleiades Publishing, 1957 77(2016), 1 vom: Jan., Seite 106-129 (DE-627)129603481 (DE-600)241725-X (DE-576)015097315 0005-1179 nnns volume:77 year:2016 number:1 month:01 pages:106-129 https://doi.org/10.1134/S0005117916010069 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-MAT GBV_ILN_70 AR 77 2016 1 01 106-129 |
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10.1134/S0005117916010069 doi (DE-627)OLC2060908876 (DE-He213)S0005117916010069-p DE-627 ger DE-627 rakwb eng 000 620 VZ Andreev, K. V. verfasserin aut Moving observer trajectory control by angular measurements in tracking problem 2016 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2016 Abstract An optimal path synthesis problem for a moving observer that performs angular observations over a target moving uniformly along a straight line on a plane is solved. It is supposed that elevation and azimuth angles can be observed when the observer moves in space and only the azimuth angle can be observed when the observer moves on a plane. Observer’s trajectories are obtained with the help of Pontryagin’smaximum principle as numerical solutions of an optimal control problem. As a performance criterion the trace of covariance matrix of the target motion elements estimate is used. A possibility of solving the problem in real time on board for unmanned aerial vehicle is investigated. A comparison with the scenario of two unmanned aerial vehicles using is given. Remote Control Optimal Control Problem Pitch Angle Unmanned Aerial Vehicle Elevation Angle Rubinovich, E. Ya. aut Enthalten in Automation and remote control Pleiades Publishing, 1957 77(2016), 1 vom: Jan., Seite 106-129 (DE-627)129603481 (DE-600)241725-X (DE-576)015097315 0005-1179 nnns volume:77 year:2016 number:1 month:01 pages:106-129 https://doi.org/10.1134/S0005117916010069 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-MAT GBV_ILN_70 AR 77 2016 1 01 106-129 |
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10.1134/S0005117916010069 doi (DE-627)OLC2060908876 (DE-He213)S0005117916010069-p DE-627 ger DE-627 rakwb eng 000 620 VZ Andreev, K. V. verfasserin aut Moving observer trajectory control by angular measurements in tracking problem 2016 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Pleiades Publishing, Ltd. 2016 Abstract An optimal path synthesis problem for a moving observer that performs angular observations over a target moving uniformly along a straight line on a plane is solved. It is supposed that elevation and azimuth angles can be observed when the observer moves in space and only the azimuth angle can be observed when the observer moves on a plane. Observer’s trajectories are obtained with the help of Pontryagin’smaximum principle as numerical solutions of an optimal control problem. As a performance criterion the trace of covariance matrix of the target motion elements estimate is used. A possibility of solving the problem in real time on board for unmanned aerial vehicle is investigated. A comparison with the scenario of two unmanned aerial vehicles using is given. Remote Control Optimal Control Problem Pitch Angle Unmanned Aerial Vehicle Elevation Angle Rubinovich, E. Ya. aut Enthalten in Automation and remote control Pleiades Publishing, 1957 77(2016), 1 vom: Jan., Seite 106-129 (DE-627)129603481 (DE-600)241725-X (DE-576)015097315 0005-1179 nnns volume:77 year:2016 number:1 month:01 pages:106-129 https://doi.org/10.1134/S0005117916010069 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-MAT GBV_ILN_70 AR 77 2016 1 01 106-129 |
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Abstract An optimal path synthesis problem for a moving observer that performs angular observations over a target moving uniformly along a straight line on a plane is solved. It is supposed that elevation and azimuth angles can be observed when the observer moves in space and only the azimuth angle can be observed when the observer moves on a plane. Observer’s trajectories are obtained with the help of Pontryagin’smaximum principle as numerical solutions of an optimal control problem. As a performance criterion the trace of covariance matrix of the target motion elements estimate is used. A possibility of solving the problem in real time on board for unmanned aerial vehicle is investigated. A comparison with the scenario of two unmanned aerial vehicles using is given. © Pleiades Publishing, Ltd. 2016 |
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Abstract An optimal path synthesis problem for a moving observer that performs angular observations over a target moving uniformly along a straight line on a plane is solved. It is supposed that elevation and azimuth angles can be observed when the observer moves in space and only the azimuth angle can be observed when the observer moves on a plane. Observer’s trajectories are obtained with the help of Pontryagin’smaximum principle as numerical solutions of an optimal control problem. As a performance criterion the trace of covariance matrix of the target motion elements estimate is used. A possibility of solving the problem in real time on board for unmanned aerial vehicle is investigated. A comparison with the scenario of two unmanned aerial vehicles using is given. © Pleiades Publishing, Ltd. 2016 |
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Abstract An optimal path synthesis problem for a moving observer that performs angular observations over a target moving uniformly along a straight line on a plane is solved. It is supposed that elevation and azimuth angles can be observed when the observer moves in space and only the azimuth angle can be observed when the observer moves on a plane. Observer’s trajectories are obtained with the help of Pontryagin’smaximum principle as numerical solutions of an optimal control problem. As a performance criterion the trace of covariance matrix of the target motion elements estimate is used. A possibility of solving the problem in real time on board for unmanned aerial vehicle is investigated. A comparison with the scenario of two unmanned aerial vehicles using is given. © Pleiades Publishing, Ltd. 2016 |
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V.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Moving observer trajectory control by angular measurements in tracking problem</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2016</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Pleiades Publishing, Ltd. 2016</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract An optimal path synthesis problem for a moving observer that performs angular observations over a target moving uniformly along a straight line on a plane is solved. It is supposed that elevation and azimuth angles can be observed when the observer moves in space and only the azimuth angle can be observed when the observer moves on a plane. Observer’s trajectories are obtained with the help of Pontryagin’smaximum principle as numerical solutions of an optimal control problem. As a performance criterion the trace of covariance matrix of the target motion elements estimate is used. A possibility of solving the problem in real time on board for unmanned aerial vehicle is investigated. A comparison with the scenario of two unmanned aerial vehicles using is given.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Remote Control</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Optimal Control Problem</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Pitch Angle</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Unmanned Aerial Vehicle</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Elevation Angle</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Rubinovich, E. Ya.</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Automation and remote control</subfield><subfield code="d">Pleiades Publishing, 1957</subfield><subfield code="g">77(2016), 1 vom: Jan., Seite 106-129</subfield><subfield code="w">(DE-627)129603481</subfield><subfield code="w">(DE-600)241725-X</subfield><subfield code="w">(DE-576)015097315</subfield><subfield code="x">0005-1179</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:77</subfield><subfield code="g">year:2016</subfield><subfield code="g">number:1</subfield><subfield code="g">month:01</subfield><subfield code="g">pages:106-129</subfield></datafield><datafield tag="856" ind1="4" ind2="1"><subfield code="u">https://doi.org/10.1134/S0005117916010069</subfield><subfield code="z">lizenzpflichtig</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_OLC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-TEC</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SSG-OLC-MAT</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">77</subfield><subfield code="j">2016</subfield><subfield code="e">1</subfield><subfield code="c">01</subfield><subfield code="h">106-129</subfield></datafield></record></collection>
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