RU93006196A - SIDE MOVEMENT MANAGEMENT SYSTEM OF UNCLEANED LOW-DIMENSIONAL AIRCRAFT - Google Patents

SIDE MOVEMENT MANAGEMENT SYSTEM OF UNCLEANED LOW-DIMENSIONAL AIRCRAFT

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Publication number
RU93006196A
RU93006196A RU93006196/24A RU93006196A RU93006196A RU 93006196 A RU93006196 A RU 93006196A RU 93006196/24 A RU93006196/24 A RU 93006196/24A RU 93006196 A RU93006196 A RU 93006196A RU 93006196 A RU93006196 A RU 93006196A
Authority
RU
Russia
Prior art keywords
uncleaned
low
management system
flight
aircraft
Prior art date
Application number
RU93006196/24A
Other languages
Russian (ru)
Other versions
RU2042170C1 (en
Inventor
Л.Г. Романенко
Г.Л. Романенко
Н.А. Шилова
Original Assignee
Л.Г. Романенко
Г.Л. Романенко
Н.А. Шилова
Filing date
Publication date
Application filed by Л.Г. Романенко, Г.Л. Романенко, Н.А. Шилова filed Critical Л.Г. Романенко
Priority to RU93006196A priority Critical patent/RU2042170C1/en
Priority claimed from RU93006196A external-priority patent/RU2042170C1/en
Application granted granted Critical
Publication of RU2042170C1 publication Critical patent/RU2042170C1/en
Publication of RU93006196A publication Critical patent/RU93006196A/en

Links

Claims (1)

Изобретение относится к области автоматического регулирования, а именно к системам управления полетом беспилотного малоразмерного летательного аппарата (МЛА), и позволяет повысить устойчивость летательного аппарата по крену. Система управления содержит два канала управления с жесткой обратной связью, в состав которых входят датчики угловых скоростей крена и рыскания, сумматоры, усилители, привод элеронов, привод руля направления, датчики положения элеронов и руля направления. Благодаря введению вычислителя значений угла крена, акселерометра, датчика скорости полета, датчика высоты полета и задатчика получена система управления боковым движением беспилотного МЛА, имеющая малые габариты и вес за счет того, что текущее значение угла крена определяется путем вычислений, позволяющая обеспечить поперечную устойчивость МЛА.The invention relates to the field of automatic control, in particular to flight control systems of an unmanned small-sized aircraft (MLA), and allows you to increase the stability of the aircraft roll. The control system contains two control channels with rigid feedback, which include angular velocity sensors of heel and yaw, adders, amplifiers, aileron drive, rudder drive, aileron position sensors and rudder. Thanks to the introduction of the heel angle calculator, accelerometer, flight speed sensor, flight altitude sensor, and setting device, a lateral movement control system for unmanned LLA was obtained, having small dimensions and weight due to the fact that the current value of the angle of lurch is determined by calculations to ensure the lateral stability of the LLA.
RU93006196A 1993-02-02 1993-02-02 System for controlling side motion of pilot-free small-size flying object RU2042170C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU93006196A RU2042170C1 (en) 1993-02-02 1993-02-02 System for controlling side motion of pilot-free small-size flying object

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU93006196A RU2042170C1 (en) 1993-02-02 1993-02-02 System for controlling side motion of pilot-free small-size flying object

Publications (2)

Publication Number Publication Date
RU2042170C1 RU2042170C1 (en) 1995-08-20
RU93006196A true RU93006196A (en) 1995-10-20

Family

ID=20136602

Family Applications (1)

Application Number Title Priority Date Filing Date
RU93006196A RU2042170C1 (en) 1993-02-02 1993-02-02 System for controlling side motion of pilot-free small-size flying object

Country Status (1)

Country Link
RU (1) RU2042170C1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2611459C1 (en) * 2015-12-29 2017-02-22 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Upgraded on-board adaptive stabilization system of aircraft lateral movement
CN111045451B (en) * 2019-12-16 2022-10-18 西安航空学院 Control system of aircraft and aircraft

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