Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representation
In this work, simplified expressions have been obtained that describe the kinematics parameters of the aircraft movement and its accelerations. These expressions are needed to obtain an optimal linear control law in order to provide movement of the aircraft using the hyperbola guidance method with a...
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| Format: | Article |
| Language: | English |
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Belarusian National Technical University
2021-10-01
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| Series: | Системный анализ и прикладная информатика |
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| Online Access: | https://sapi.bntu.by/jour/article/view/519 |
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| _version_ | 1832557343530811392 |
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| author | V. V. Legkostup |
| author_facet | V. V. Legkostup |
| author_sort | V. V. Legkostup |
| collection | DOAJ |
| description | In this work, simplified expressions have been obtained that describe the kinematics parameters of the aircraft movement and its accelerations. These expressions are needed to obtain an optimal linear control law in order to provide movement of the aircraft using the hyperbola guidance method with a time difference of arrival navigation system. The key feature of the hyperbola navigation method is the ability to reduce the number of navigation positions by one when the on-board navigation equipment operates in a passive mode, carrying out only the reception of navigation information, like consumers of satellite navigation information. |
| format | Article |
| id | doaj-art-ecf0efc3c7874a2a9105c0179dafe104 |
| institution | Kabale University |
| issn | 2309-4923 2414-0481 |
| language | English |
| publishDate | 2021-10-01 |
| publisher | Belarusian National Technical University |
| record_format | Article |
| series | Системный анализ и прикладная информатика |
| spelling | doaj-art-ecf0efc3c7874a2a9105c0179dafe1042025-02-03T05:16:54ZengBelarusian National Technical UniversityСистемный анализ и прикладная информатика2309-49232414-04812021-10-0103152410.21122/2309-4923-2021-3-15-24392Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representationV. V. Legkostup0«ALEVKURP» JSCIn this work, simplified expressions have been obtained that describe the kinematics parameters of the aircraft movement and its accelerations. These expressions are needed to obtain an optimal linear control law in order to provide movement of the aircraft using the hyperbola guidance method with a time difference of arrival navigation system. The key feature of the hyperbola navigation method is the ability to reduce the number of navigation positions by one when the on-board navigation equipment operates in a passive mode, carrying out only the reception of navigation information, like consumers of satellite navigation information.https://sapi.bntu.by/jour/article/view/519curvilinear elliptic coordinate systemlame coefficientsnavigationkinematics of navigation and guidanceuavtdoa |
| spellingShingle | V. V. Legkostup Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representation Системный анализ и прикладная информатика curvilinear elliptic 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 in alternative representation |
| title_full | Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representation |
| title_fullStr | Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representation |
| title_full_unstemmed | Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representation |
| title_short | Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representation |
| title_sort | methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representation |
| topic | curvilinear elliptic coordinate system lame coefficients navigation kinematics of navigation and guidance uav tdoa |
| url | https://sapi.bntu.by/jour/article/view/519 |
| work_keys_str_mv | AT vvlegkostup methodologyofdeterminingofthetransferfunctionofengagementkinematicsofaccelerationsofanaircraftanditsellipticcoordinatesinalternativerepresentation |