Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrival
This paper discusses the problem of determining a kinematics (in terms of transfer function, as far as possible) of parameters of the motion of an aircraft expressed in the curvilinear coordinate system and control accelerations expressed in a rectangular coordinate system. Examples of curvilinear c...
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| Format: | Article |
| Language: | English |
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Belarusian National Technical University
2021-04-01
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| Series: | Системный анализ и прикладная информатика |
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| Online Access: | https://sapi.bntu.by/jour/article/view/498 |
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| author | V. V. Legkostup V. E. Markevich |
| author_facet | V. V. Legkostup V. E. Markevich |
| author_sort | V. V. Legkostup |
| collection | DOAJ |
| description | This paper discusses the problem of determining a kinematics (in terms of transfer function, as far as possible) of parameters of the motion of an aircraft expressed in the curvilinear coordinate system and control accelerations expressed in a rectangular coordinate system. Examples of curvilinear coordinate systems using in practice can be polar, biangular, two-center bipolar, elliptic, parabolic cylindrical, spherical, ellipsoidal, coordinate systems. A technique for obtaining a kinematic link for the control problem of an unmanned aerial vehicle in the elliptic coordinate system was described. It allowed to obtain simpler view of the kinematic link which could provide navigation an aircraft along the hyperbola deriving from the time difference of arrival navigation system. It can. As a result, it is possible to reduce the number of the navigation radio beacons. |
| format | Article |
| id | doaj-art-dc7204d1ac2a49939dbb9fe71fcb924d |
| institution | Kabale University |
| issn | 2309-4923 2414-0481 |
| language | English |
| publishDate | 2021-04-01 |
| publisher | Belarusian National Technical University |
| record_format | Article |
| series | Системный анализ и прикладная информатика |
| spelling | doaj-art-dc7204d1ac2a49939dbb9fe71fcb924d2025-08-20T03:38:30ZengBelarusian National Technical UniversityСистемный анализ и прикладная информатика2309-49232414-04812021-04-0101122010.21122/2309-4923-2021-1-12-20374Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrivalV. V. Legkostup0V. E. Markevich1ALEVKURP JSCSAMERA LLCThis paper discusses the problem of determining a kinematics (in terms of transfer function, as far as possible) of parameters of the motion of an aircraft expressed in the curvilinear coordinate system and control accelerations expressed in a rectangular coordinate system. Examples of curvilinear coordinate systems using in practice can be polar, biangular, two-center bipolar, elliptic, parabolic cylindrical, spherical, ellipsoidal, coordinate systems. A technique for obtaining a kinematic link for the control problem of an unmanned aerial vehicle in the elliptic coordinate system was described. It allowed to obtain simpler view of the kinematic link which could provide navigation an aircraft along the hyperbola deriving from the time difference of arrival navigation system. It can. As a result, it is possible to reduce the number of the navigation radio beacons.https://sapi.bntu.by/jour/article/view/498curvilinear coordinate systemlame coefficientsnavigationkinematics of navigation and guidanceuavtdoa |
| spellingShingle | V. V. Legkostup V. E. Markevich Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrival Системный анализ и прикладная информатика curvilinear coordinate system lame coefficients navigation kinematics of navigation and guidance uav tdoa |
| title | Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrival |
| title_full | Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrival |
| title_fullStr | Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrival |
| title_full_unstemmed | Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrival |
| title_short | Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrival |
| title_sort | methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrival |
| topic | curvilinear coordinate system lame coefficients navigation kinematics of navigation and guidance uav tdoa |
| url | https://sapi.bntu.by/jour/article/view/498 |
| work_keys_str_mv | AT vvlegkostup methodologyofdeterminingofthetransferfunctionofengagementkinematicsofaccelerationsofanaircraftanditsellipticcoordinatesusedforthrguidancebasedontimedifferenceofarrival AT vemarkevich methodologyofdeterminingofthetransferfunctionofengagementkinematicsofaccelerationsofanaircraftanditsellipticcoordinatesusedforthrguidancebasedontimedifferenceofarrival |