RU2013117643A - METHOD FOR ADAPTIVE ROUTE CONTROL OF PILOTED AIRCRAFT - Google Patents

METHOD FOR ADAPTIVE ROUTE CONTROL OF PILOTED AIRCRAFT Download PDF

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Publication number
RU2013117643A
RU2013117643A RU2013117643/11A RU2013117643A RU2013117643A RU 2013117643 A RU2013117643 A RU 2013117643A RU 2013117643/11 A RU2013117643/11 A RU 2013117643/11A RU 2013117643 A RU2013117643 A RU 2013117643A RU 2013117643 A RU2013117643 A RU 2013117643A
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flight
route
aircraft
mission
refinement
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RU2013117643/11A
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Russian (ru)
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RU2568161C2 (en
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Виктор Семенович Марусин
Олег Георгиевич Столяров
Сергей Владимирович Ярошенко
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Открытое акционерное общество "Особое конструкторское бюро "Пеленг"
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Priority to RU2013117643/11A priority Critical patent/RU2568161C2/en
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Abstract

1. Способ адаптивно-маршрутного управления пилотируемыми летательными аппаратами, основанный на обходе известных зон поражения зенитных ракетных комплексов противовоздушной обороны, включающий выполняемые на этапе планирования боевых действий процедуры расчета маршрута полета, формирования и доведения до экипажа полетного задания, а также выполняемые в ходе полета летательного аппарата процедуры последующего уточнения маршрута и полетного задания, и отличающийся тем, что маршрут полета рассчитывают, исходя из условия обеспечения наибольшей вероятности выполнения поставленной задачи и последующего возвращения летательного аппарата на аэродром посадки, достижимой для существующей тактической обстановки и ограниченности имеющегося запаса топлива.2. Способ по п.1, отличающийся тем, что уточнение маршрута полета и полетного задания выполняют на основе актуальных данных, получаемых от информационных средств, о возможных изменениях состава и дислокации зенитных ракетных комплексов, об изменении координат атакуемой цели и об отклонении летательного аппарата от рассчитанного маршрута.1. The method of adaptive-route control of manned aircraft based on bypassing the known zones of destruction of anti-aircraft missile systems of air defense, including procedures for calculating the flight route performed at the stage of combat operations planning, formation and delivery of the flight mission to the crew, as well as performed during the flight apparatus procedures for the subsequent refinement of the route and flight mission, and characterized in that the flight route is calculated based on the conditions the greatest likelihood of accomplishing the task and the subsequent return of the aircraft to the landing aerodrome, achievable for the existing tactical situation and the limited availability of fuel. 2. The method according to claim 1, characterized in that the refinement of the flight route and flight mission is performed on the basis of relevant data received from information tools, about possible changes in the composition and deployment of anti-aircraft missile systems, about a change in the coordinates of the target and about the deviation of the aircraft from the calculated route .

Claims (2)

1. Способ адаптивно-маршрутного управления пилотируемыми летательными аппаратами, основанный на обходе известных зон поражения зенитных ракетных комплексов противовоздушной обороны, включающий выполняемые на этапе планирования боевых действий процедуры расчета маршрута полета, формирования и доведения до экипажа полетного задания, а также выполняемые в ходе полета летательного аппарата процедуры последующего уточнения маршрута и полетного задания, и отличающийся тем, что маршрут полета рассчитывают, исходя из условия обеспечения наибольшей вероятности выполнения поставленной задачи и последующего возвращения летательного аппарата на аэродром посадки, достижимой для существующей тактической обстановки и ограниченности имеющегося запаса топлива.1. The method of adaptive-route control of manned aircraft based on bypassing the known zones of destruction of anti-aircraft missile systems of air defense, including procedures for calculating the flight route performed at the stage of combat operations planning, formation and delivery of the flight mission to the crew, as well as performed during the flight apparatus procedures for the subsequent refinement of the route and flight mission, and characterized in that the flight route is calculated based on the conditions the greatest likelihood of completing the task and the subsequent return of the aircraft to the landing aerodrome, achievable for the existing tactical situation and the limited availability of fuel. 2. Способ по п.1, отличающийся тем, что уточнение маршрута полета и полетного задания выполняют на основе актуальных данных, получаемых от информационных средств, о возможных изменениях состава и дислокации зенитных ракетных комплексов, об изменении координат атакуемой цели и об отклонении летательного аппарата от рассчитанного маршрута. 2. The method according to claim 1, characterized in that the refinement of the flight route and flight mission is performed on the basis of current data received from information tools, about possible changes in the composition and deployment of anti-aircraft missile systems, about changes in the coordinates of the target and about the deviation of the aircraft from calculated route.
RU2013117643/11A 2013-04-16 2013-04-16 Method for adaptive-route control of manned aircraft RU2568161C2 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
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CN107703971A (en) * 2017-11-20 2018-02-16 唐菲菲 Unmanned aerial vehicle maneuvering method and system for inspection area

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2726512C2 (en) * 2018-05-17 2020-07-14 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МО РФ Method for trajectories of high-speed unmanned aerial vehicles in the area of countermeasures arrangement
RU2723783C1 (en) * 2019-08-07 2020-06-17 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Method of cruise missile homing
RU2734171C1 (en) * 2020-04-29 2020-10-13 Акционерное общество "Уральское производственное предприятие "Вектор" (АО "УПП "Вектор") Method for optimum adaptation of an air target intercept route when a group of air defence systems is in the area of flights

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RU2316023C2 (en) * 2005-12-06 2008-01-27 Открытое акционерное общество "Корпорация "Фазотрон - научно-исследовательский институт радиостроения" Method for optimal avoidance of thunderstorm
RU74493U1 (en) * 2008-03-25 2008-06-27 Борис Николаевич Горевич SYSTEM OF CONTROL OF JOINT ACTIONS OF AVIATION AND ANTI-AIR MANAGEMENT PLACES IN THE FIRE AREA OF ANTI-AIR MANAGEMENT ARMS
RU2444044C1 (en) * 2010-10-13 2012-02-27 Открытое акционерное общество "Раменское приборостроительное конструкторское бюро" (ОАО "РПКБ") Device to control trajectory of aircraft when flying along route

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107703971A (en) * 2017-11-20 2018-02-16 唐菲菲 Unmanned aerial vehicle maneuvering method and system for inspection area
CN107703971B (en) * 2017-11-20 2023-08-25 唐菲菲 Unmanned aerial vehicle mobilization method and unmanned aerial vehicle mobilization system for patrol area

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