METHOD OF GENERATING SIGNAL FOR AIRCRAFT LATERAL GUIDANCE AND DEVICE FOR IMPLEMENTING METHOD Russian patent published in 2008 - IPC G05D1/00 

Abstract RU 2339990 C1

FIELD: physics.

SUBSTANCE: device has a apparatus for selecting the lateral guidance signal, two subtraction elements, two adder amplifiers, two signal limiters, piecewise linear function information transducer, aperiodic filter, inverting amplifier, sensors for course angle, course angular velocity, angle of bank and banking angular velocity. The lateral guidance output signal is generated through limiting the resultant course signal. There is additional generation of a modular function signal as a sum of relay and non-linear components of the lateral guidance signal. The reference roll guidance signal is set to be equal to the lateral guidance signal when the modular function signal exceeds the given value.

EFFECT: wider functional capabilities and increased accuracy of control.

2 cl, 4 dwg

Similar patents RU2339990C1

Title Year Author Number
ADAPTIVE DEVICE OF AIRCRAFT COORDINATED CONTROL 2008
  • Syrov Antolij Sergeevich
  • Puchkov Aleksandr Mikhajlovich
  • Skabitskij Vladimir Ivanovich
  • Kareva Elena Mikhajlovna
RU2367993C1
AIRCRAFT DUAL CHANNEL COORDINATED CONTROLLER 2013
  • Syrov Anatolij Sergeevich
  • Puchkov Aleksandr Mikhajlovich
RU2532720C1
ADAPTIVE DEVICE OF AIRCRAFT COORDINATED CONTROL 2008
  • Syrov Anatolij Sergeevich
  • Puchkov Aleksandr Mikhajlovich
  • Petushkov Boris Konstantinovich
  • Cherepanova Valentina Evgen'Evna
  • Kareva Elena Mikhajlovna
RU2367992C1
AIRCRAFT ADAPTIVE COORDINATED CONTROLLER 2014
  • Puchkov Aleksandr Mikhajlovich
  • Seleznev Anton Evgen'Evich
  • Khlopkin Artem Vladimirovich
  • Solov'Ev Aleksej Sergeevich
RU2554515C1
METHOD FOR FORMING LATERAL-DIRECTIONAL SIGNALS OF NON-STATIONARY UNMANNED AERIAL VEHICLE WITH ADAPTIVE-FUNCTIONAL CORRECTION AND A DEVICE FOR ITS IMPLEMENTATION 2016
  • Syrov Anatolij Sergeevich
  • Puchkov Aleksandr Mikhajlovich
  • Zhdanovich Nadezhda Pavlovna
  • Solovev Aleksej Sergeevich
  • Seleznev Anton Evgenevich
  • Romanov Oleg Dmitrievich
  • Khlopkin Artem Vladimirovich
RU2631736C1
METHOD OF GENERATING DIGITAL/ANALOGUE SIGNAL FOR STABILISING ANGULAR POSITION OF AIRCRAFT ON HEADING AND APPARATUS FOR REALISING SAID METHOD 2012
  • Syrov Anatolij Sergeevich
  • Zhdanovich Nadezhda Pavlovna
  • Kravchuk Sergej Valentinovich
  • Petrov Andrej Borisovich
  • Puchkov Aleksandr Mikhajlovich
  • Tatsjuk Dmitrij Grigor'Evich
  • Cherepanova Valentina Evgen'Evna
RU2491602C1
CONTROL DEVICE FOR SYSTEM OF COORDINATED CONTROL OF FLIGHT VEHICLE 2003
  • Kravchuk S.V.
  • Puchkov A.M.
  • Syrov A.S.
RU2237269C1
METHOD OF GENERATING DIGITAL/ANALOGUE ADAPTIVE SIGNAL FOR STABILISING ANGULAR POSITION OF AIRCRAFT ON HEADING AND APPARATUS FOR REALISING SAID METHOD 2012
  • Syrov Anatolij Sergeevich
  • Zhdanovich Nadezhda Pavlovna
  • Lasunin Il'Ja Vladimirovich
  • Nikiforov Pavel Nikolaevich
  • Puchkov Aleksandr Mikhajlovich
  • Tarasov Vladimir Il'Ich
  • Firsov Sergej Aleksandrovich
RU2491600C1
ADAPTIVE SYSTEM FOR CONTROLLING FLIGHT HEIGHT OF AN AIRCRAFT 2005
  • Syrov Anatolij Sergeevich
  • Trusov Vladimir Nikolaevich
  • Larionov Vitalij Aleksandrovich
  • Abadeev Ehduard Matveevich
  • Dubinkin Igor' Mikhajlovich
  • Kravchuk Sergej Valentinovich
  • Makarov Nikolaj Valentinovich
  • Puchkov Aleksandr Mikhajlovich
RU2279119C1
SYSTEM FOR CONTROLLING ANGULAR MOTION OF PILOT -FREE AIRCRAFT 2003
  • Bonk R.I.
  • Petushkov B.K.
  • Puchkov A.M.
  • Syrov A.S.
  • Cherepanova V.E.
RU2234117C1

RU 2 339 990 C1

Authors

Abadeev Ehduard Matveevich

Ezhov Vladimir Vasil'Evich

Kravchuk Sergej Valentinovich

Ljapunov Vladimir Viktorovich

Makarov Nikolaj Valentinovich

Puchkov Aleksandr Mikhajlovich

Syrov Anatolij Sergeevich

Trusov Vladimir Nikolaevich

Dates

2008-11-27Published

2007-06-14Filed