title: On One Problem of Controlling an Airplane-type Unmanned Aerial Vehicle with Given Intermediate Values of Different Parts of Coordinates
metadata.name: dc.contributor.author
metadata.value: Barseghyan, Vanya Rafaelovich
metadata.lang: -
metadata.name: dc.contributor.author
metadata.value: Matevosyan, Aram Gagikovich
metadata.lang: -
metadata.name: dc.date.accessioned
metadata.value: 2023-07-04T14:38:08Z
metadata.lang: -
metadata.name: dc.date.available
metadata.value: 2023-07-04T14:38:08Z
metadata.lang: -
metadata.name: dc.date.issued
metadata.value: 2023-06
metadata.lang: -
metadata.name: dc.identifier.other
metadata.value: https://doi.org/10.21638/11701/spbu35.2023.205
metadata.lang: -
metadata.name: dc.identifier.uri
metadata.value: http://hdl.handle.net/11701/41730
metadata.lang: -
metadata.name: dc.description.abstract
metadata.value: The mathematical model of spatial flight of an unmanned airplane-type vehicle is considered. For a linearized mathematical model of an unmanned aerial vehicle the problem of synthesis of control laws with given initial, finite values of the phase vector and intermediate values of different parts of coordinates at different moments of time is solved. A necessary and sufficient condition for the existence of program control and the corresponding motion is formulated. The control functions and corresponding phase trajectories of motion are constructed. As an application of the proposed approach, explicit expressions of the program control function and program motion are constructed for specific numerical values.
metadata.lang: en_GB
metadata.name: dc.language.iso
metadata.value: ru
metadata.lang: en_GB
metadata.name: dc.publisher
metadata.value: St Petersburg State University
metadata.lang: en_GB
metadata.name: dc.relation.ispartofseries
metadata.value: Differential Equations and Control Processes;Issue 2
metadata.lang: -
metadata.name: dc.subject
metadata.value: unmanned aerial vehicle
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: flight control
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: intermediate conditions
metadata.lang: en_GB
metadata.name: dc.subject
metadata.value: phase trajectories
metadata.lang: en_GB
metadata.name: dc.title
metadata.value: On One Problem of Controlling an Airplane-type Unmanned Aerial Vehicle with Given Intermediate Values of Different Parts of Coordinates
metadata.lang: en_GB
metadata.name: dc.type
metadata.value: Article
metadata.lang: en_GB
resources.filename: 86-96.pdf
resources.url: https://dspace.spbu.ru/bitstream/11701/41730/1/86-96.pdf
resources.format: Adobe PDF
resources.size: 713,92 kB