RU2209747C2 - Pilot display - Google Patents

Pilot display Download PDF

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Publication number
RU2209747C2
RU2209747C2 RU2001123259A RU2001123259A RU2209747C2 RU 2209747 C2 RU2209747 C2 RU 2209747C2 RU 2001123259 A RU2001123259 A RU 2001123259A RU 2001123259 A RU2001123259 A RU 2001123259A RU 2209747 C2 RU2209747 C2 RU 2209747C2
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RU
Russia
Prior art keywords
input
inputs
output
multiplier unit
indicator
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RU2001123259A
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Russian (ru)
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RU2001123259A (en
Inventor
А.В. Бабиченко
М.И. Орехов
И.В. Радченко
В.К. Шкред
Original Assignee
Открытое акционерное общество "Раменское приборостроительное конструкторское бюро"
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Priority to RU2001123259A priority Critical patent/RU2209747C2/en
Publication of RU2001123259A publication Critical patent/RU2001123259A/en
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Abstract

FIELD: pilot instrumentation and complexes. SUBSTANCE: proposed pilot display includes indicator whose two inputs are connected to on-board information system receiving normal and side components of phantom acceleration of object. Besides that proposed device includes the following units connected in series: sine- cosine transducer, multiplier unit, summing amplifier, aperiodic member and integrating amplifier. Output of integrating amplifier is connected to input of indicator and to input of sine-cosine transducer whose second output is connected to second input of multiplier unit. Second output of multiplier unit is connected to second input of summing amplifier. Third and fourth inputs of multiplier unit are used as inputs of pilot display. Motion of indicator does not depend on angular velocity and longitudinal acceleration of flying vehicle as well as on friction forces; it is required function of normal and side phantom acceleration. EFFECT: enhanced operational stability; avoidance of methodical error in readings. 1 dwg

Description

Текст описания в факсимильном виде (см. чертежи)й Description text in facsimile form (see drawings)

Claims (1)

Пилотажный индикатор скольжения, содержащий указатель и подключенный к бортовой информационной системе двумя входами, на которые поступают нормальная и боковая составляющие кажущегося ускорения объекта, отличающийся тем, что он содержит последовательно соединенные синусно-косинусный преобразователь, блок умножения, суммирующий усилитель, апериодическое звено, интегрирующий усилитель, выход которого подключен ко входу указателя и ко входу синусно-косинусного преобразователя, второй выход которого подключен ко второму входу блока умножения, второй выход которого подключен ко второму входу суммирующего усилителя, при этом входами пилотажного индикатора скольжения являются третий и четвертый входы блока умножения. An aerobatic glide indicator containing a pointer and connected to the on-board information system by two inputs to which the normal and lateral components of the apparent acceleration of the object are received, characterized in that it contains serially connected sine-cosine transducer, multiplication unit, summing amplifier, aperiodic link, integrating amplifier whose output is connected to the input of the pointer and to the input of the sine-cosine converter, the second output of which is connected to the second input of the block multiplication, the second output of which is connected to the second input of the summing amplifier, the inputs of a flight slip indicator are third and fourth inputs of the multiplication block.
RU2001123259A 2001-08-21 2001-08-21 Pilot display RU2209747C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2001123259A RU2209747C2 (en) 2001-08-21 2001-08-21 Pilot display

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2001123259A RU2209747C2 (en) 2001-08-21 2001-08-21 Pilot display

Publications (2)

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RU2001123259A RU2001123259A (en) 2003-07-10
RU2209747C2 true RU2209747C2 (en) 2003-08-10

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RU2001123259A RU2209747C2 (en) 2001-08-21 2001-08-21 Pilot display

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Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
МИХАЙЛОВ О.И. и др. Авиационные приборы. - М.: Машиностроение, 1977, с.113-115. *

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20170822