SU330458A1 - COMPUTER DEVICE - Google Patents

COMPUTER DEVICE

Info

Publication number
SU330458A1
SU330458A1 SU1321067/24A SU1321067A SU330458A1 SU 330458 A1 SU330458 A1 SU 330458A1 SU 1321067/24 A SU1321067/24 A SU 1321067/24A SU 1321067 A SU1321067 A SU 1321067A SU 330458 A1 SU330458 A1 SU 330458A1
Authority
SU
USSR - Soviet Union
Prior art keywords
input
adder
aircraft
block
amplifying
Prior art date
Application number
SU1321067/24A
Other languages
Russian (ru)
Inventor
А.И. Брук
Л.Д. Брыкова
И.М. Евстигнеева
М.В. Иванова
Л.Л. Николаев
Ю.С. Розенфельд
Ф.А. Фурман
Original Assignee
А.И. Брук
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by А.И. Брук filed Critical А.И. Брук
Priority to SU1321067/24A priority Critical patent/SU330458A1/en
Application granted granted Critical
Publication of SU330458A1 publication Critical patent/SU330458A1/en

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Вычислительное устройство для управления боковым движением летательного аппарата при его стабилизации на заданной траектории, содержащее усилительные, дифференцирующий блоки и сумматор на выходе устройства, связанный непосредственно с блоком типа "насыщение" и через усилительный блок - с первым входом устройства, который подсоединен к датчику отклонения летательного аппарата от заданного курса, а ко второму входу устройства подключен датчик отклонения летательного аппарата от заданной траектории, отличающееся тем, что, с целью увеличения допустимых в диапазонах углов сноса и ошибок выставки заданного курса, на входе нелинейного блока включен второй сумматор, один вход которого через усилительное звено с инвертором соединен с первым входом устройства, а второй вход сумматора через другой усилительный блок связан со вторым входом устройства, через дифференцирующий блок соединенным с сумматором на выходе устройства.A computing device for controlling lateral movement of the aircraft during its stabilization on a given trajectory, containing amplifying, differentiating blocks and an adder at the output of the device, connected directly to the block of "saturation" type and through the amplifying block to the first input of the device, which is connected to the aircraft deviation sensor device from the specified course, and a sensor deviation of the aircraft from the specified path is connected to the second input of the device, characterized in that the admissions in a range of drift angles and exhibition errors of a given course, the second adder is connected to the input of the nonlinear unit, one input of which is connected to the first input of the device through an amplifier link, and the second input of the adder through another amplifying block is connected to the second input of the device unit connected to the adder at the output of the device.

SU1321067/24A 1969-02-24 1969-02-24 COMPUTER DEVICE SU330458A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1321067/24A SU330458A1 (en) 1969-02-24 1969-02-24 COMPUTER DEVICE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1321067/24A SU330458A1 (en) 1969-02-24 1969-02-24 COMPUTER DEVICE

Publications (1)

Publication Number Publication Date
SU330458A1 true SU330458A1 (en) 2005-07-27

Family

ID=60514742

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1321067/24A SU330458A1 (en) 1969-02-24 1969-02-24 COMPUTER DEVICE

Country Status (1)

Country Link
SU (1) SU330458A1 (en)

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