FR2397001A1 - Capteur de signal d'erreur a inertie et pilote automatique associe - Google Patents

Capteur de signal d'erreur a inertie et pilote automatique associe

Info

Publication number
FR2397001A1
FR2397001A1 FR7721592A FR7721592A FR2397001A1 FR 2397001 A1 FR2397001 A1 FR 2397001A1 FR 7721592 A FR7721592 A FR 7721592A FR 7721592 A FR7721592 A FR 7721592A FR 2397001 A1 FR2397001 A1 FR 2397001A1
Authority
FR
France
Prior art keywords
flip
flop
pulses
pick
comparator
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
FR7721592A
Other languages
English (en)
Other versions
FR2397001B1 (fr
Inventor
Joseph De Grivel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bpifrance Financement SA
Original Assignee
Agence National de Valorisation de la Recherche ANVAR
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 Agence National de Valorisation de la Recherche ANVAR filed Critical Agence National de Valorisation de la Recherche ANVAR
Priority to FR7721592A priority Critical patent/FR2397001A1/fr
Priority to DE19782829049 priority patent/DE2829049A1/de
Publication of FR2397001A1 publication Critical patent/FR2397001A1/fr
Application granted granted Critical
Publication of FR2397001B1 publication Critical patent/FR2397001B1/fr
Granted legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
    • G05D1/0033—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement by having the operator tracking the vehicle either by direct line of sight or via one or more cameras located remotely from the vehicle
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H30/00—Remote-control arrangements specially adapted for toys, e.g. for toy vehicles
    • A63H30/02—Electrical arrangements
    • A63H30/04—Electrical arrangements using wireless transmission
    • G—PHYSICS
    • G08—SIGNALLING
    • G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
    • G08C19/00—Electric signal transmission systems
    • G08C19/16—Electric signal transmission systems in which transmission is by pulses
    • G08C19/22—Electric signal transmission systems in which transmission is by pulses by varying the duration of individual pulses

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Control Of Turbines (AREA)
  • Toys (AREA)

Abstract

Dispositif de pilotage automatique pour engin volant comprenant un récepteur embarqué à cinq voies V1 à V5 dont deux d'entre elles V1 et V4 , commandent respectivement le régime du moteur et le gouvernail de direction. b. Deux voies V 2 et V3 servent à tarer par décalage de zéro au moyen de comparateurs K2 et K3 les signaux produits dans des monostables à créneau variable M2 et M3 par des capteurs de tangage et de roulis, et une voie V 5 agit sur un commutateur 20 permettant de passer du pilotage manuel au pilotage automatique et inversement. c. Facilite le pilotage des maquettes d'avion.
FR7721592A 1977-07-07 1977-07-07 Capteur de signal d'erreur a inertie et pilote automatique associe Granted FR2397001A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR7721592A FR2397001A1 (fr) 1977-07-07 1977-07-07 Capteur de signal d'erreur a inertie et pilote automatique associe
DE19782829049 DE2829049A1 (de) 1977-07-07 1978-07-01 Traegheits-fehlersignal-aufnehmer mit angegliederter automatik-steuerung

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7721592A FR2397001A1 (fr) 1977-07-07 1977-07-07 Capteur de signal d'erreur a inertie et pilote automatique associe

Publications (2)

Publication Number Publication Date
FR2397001A1 true FR2397001A1 (fr) 1979-02-02
FR2397001B1 FR2397001B1 (fr) 1981-01-30

Family

ID=9193337

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7721592A Granted FR2397001A1 (fr) 1977-07-07 1977-07-07 Capteur de signal d'erreur a inertie et pilote automatique associe

Country Status (2)

Country Link
DE (1) DE2829049A1 (fr)
FR (1) FR2397001A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995030180A1 (fr) * 1994-04-29 1995-11-09 Lodge Flying Ltd. Stabilisation d'un avion radiocommande
WO1998014253A1 (fr) * 1996-10-02 1998-04-09 Gm Racing Modellsportvertrieb Gmbh Dispositif pour agir sur la qualite de conduite de vehicules en modeles reduits telecommandes

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995030180A1 (fr) * 1994-04-29 1995-11-09 Lodge Flying Ltd. Stabilisation d'un avion radiocommande
WO1998014253A1 (fr) * 1996-10-02 1998-04-09 Gm Racing Modellsportvertrieb Gmbh Dispositif pour agir sur la qualite de conduite de vehicules en modeles reduits telecommandes
US6241574B1 (en) 1996-10-02 2001-06-05 Ralf Helbing Device to influence the driving performance of a remote-controlled model vehicle

Also Published As

Publication number Publication date
FR2397001B1 (fr) 1981-01-30
DE2829049A1 (de) 1979-02-01

Similar Documents

Publication Publication Date Title
MY8500787A (en) Deflecting device for cathode ray-tube
FR2397001A1 (fr) Capteur de signal d'erreur a inertie et pilote automatique associe
GB1535560A (en) Automatic control circuitry
SE8200637L (sv) Horisontalavbojningskrets med tva arbetssett
GB1515408A (en) Electrical delay devices
AU3124484A (en) Digital echo cancellation
US2517579A (en) Multichannel pulse receiving system
JPS5336412A (en) Synchronous lead-in system for false 4-phase modulation signal
JPS5458179A (en) Self-correcting type control apparatus
JPS57107688A (en) Sampling pulse correcting system
JPS5373324A (en) Controlling device of pulse width controller inverters
JPS57171212A (en) Capacity type converter
JPS5326527A (en) Index signal generating equi pment
SU678297A2 (ru) Устройство дл записи фазового сдвига характеристик при измен ющейс частоте колебаний рычагов управлени летательного аппарата
JPH02154179A (ja) 自動利得制御装置
GB2203304A (en) Local-oscillator system
JPS543489A (en) Receiver for phase difference navigation use
JPS552927A (en) Automatic time correction device
GB2044489A (en) X-ray tube arrangements
SU151696A1 (ru) Устройство дл коррекции сигналов, искаженных переходными процессами
US3005051A (en) Noise elimination in multiplex transmission systems working according to the time division principle
JPS5621481A (en) Automatic gain control circuit
UPADHYAYA et al. Adaptive optimal input synthesis for linear system identification[Interim Report]
JPS5310294A (en) Automatic gain control circuit
JPS53105960A (en) Automatic amplitude equalizer

Legal Events

Date Code Title Description
ST Notification of lapse