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: | Sistemnyj Analiz i Prikladnaâ Informatika |
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| Online Access: | https://sapi.bntu.by/jour/article/view/519 |
| _version_ | 1797873753817874432 |
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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. |
| first_indexed | 2024-04-10T01:20:09Z |
| format | Article |
| id | doaj.art-ecf0efc3c7874a2a9105c0179dafe104 |
| institution | Directory Open Access Journal |
| issn | 2309-4923 2414-0481 |
| language | English |
| last_indexed | 2024-04-10T01:20:09Z |
| publishDate | 2021-10-01 |
| publisher | Belarusian National Technical University |
| record_format | Article |
| series | Sistemnyj Analiz i Prikladnaâ Informatika |
| spelling | doaj.art-ecf0efc3c7874a2a9105c0179dafe1042023-03-13T09:47:42ZengBelarusian National Technical UniversitySistemnyj Analiz i Prikladnaâ Informatika2309-49232414-04812021-10-0103152410.21122/2309-4923-2021-3-15-24392Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representationV. V. Legkostup0«АЛЕВКУРП» ОАОIn 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/519эллиптическая криволинейная система координаткоэффициенты ламеразностно-дальномерная системанавигациякинематическая связьбеспилотный летательный аппарат (бла)оптимальное линейное управление |
| 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 Sistemnyj Analiz i Prikladnaâ Informatika эллиптическая криволинейная система координат коэффициенты ламе разностно-дальномерная система навигация кинематическая связь беспилотный летательный аппарат (бла) оптимальное линейное управление |
| 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 | эллиптическая криволинейная система координат коэффициенты ламе разностно-дальномерная система навигация кинематическая связь беспилотный летательный аппарат (бла) оптимальное линейное управление |
| url | https://sapi.bntu.by/jour/article/view/519 |
| work_keys_str_mv | AT vvlegkostup methodologyofdeterminingofthetransferfunctionofengagementkinematicsofaccelerationsofanaircraftanditsellipticcoordinatesinalternativerepresentation |