DE29500702U1 - Optical autopilot - Google Patents

Optical autopilot

Info

Publication number
DE29500702U1
DE29500702U1 DE29500702U DE29500702U DE29500702U1 DE 29500702 U1 DE29500702 U1 DE 29500702U1 DE 29500702 U DE29500702 U DE 29500702U DE 29500702 U DE29500702 U DE 29500702U DE 29500702 U1 DE29500702 U1 DE 29500702U1
Authority
DE
Germany
Prior art keywords
autopilot
optical
model aircraft
flight attitude
control
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.)
Expired - Lifetime
Application number
DE29500702U
Other languages
German (de)
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.)
JAMARA MODELLTECHNIK INH ERICH
Original Assignee
JAMARA MODELLTECHNIK INH ERICH
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 JAMARA MODELLTECHNIK INH ERICH filed Critical JAMARA MODELLTECHNIK INH ERICH
Priority to DE29500702U priority Critical patent/DE29500702U1/en
Publication of DE29500702U1 publication Critical patent/DE29500702U1/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Glass Compositions (AREA)
  • Photoreceptors In Electrophotography (AREA)
  • Optical Communication System (AREA)

Description

Qebrauchsmusteranmeldung optische*·" Autopilot,Utility model application optical*·" autopilot,

Die Erfindung betrifft einen Autopilot nach dem Gattungsbegriff des Schutzanspruchs 1. Geräte dieser Art werden zur automatischen Fluglageregelung bei ferngesteuerten^Modellflugzeugen eingesetzt. Uobei die Fluglage über das Querruder und Höhenruder stabilisiert- Diese wiederum werden über die an der Autopilotelektronik angeschlossenen Servos(3 u-4) angesteuert. Als .Informationsquelle des Autopilot dient ein optischer Differentialgeber(2),welcher außerhalb unten am Rumpf des Modellflugzeuges angebracht wird.
Die Gebersignale sind proportional zumThe invention relates to an autopilot according to the generic term of claim 1. Devices of this type are used for automatic flight attitude control in remote-controlled model aircraft. The flight attitude is stabilized via the ailerons and elevator. These in turn are controlled via the servos (3 and 4) connected to the autopilot electronics. An optical differential sensor (2) serves as the information source for the autopilot, which is attached to the bottom of the fuselage of the model aircraft.
The encoder signals are proportional to the

Neigungswinkel des Modells bezogen auf den optischen Horizont. Der Autopilot kann mit jedem Fernsteuersystem benutzt werden welches einen positiven Steuerimpuls mit positiver Polarität hat. Der Autopilot kann per Fernbedienung mit welcher auch das Modellflugzeug gesteuert wird ein oder ausgeschaltet werden.In eingeschaltetem Zustand werden die Autopilotsignale durch die Signale der Fernsteuerung übersteuert. Lässt der Pilot alle Steuerhebel seiner Fernsteuerung los, so bringt der optische Fluglageregler das Flugmodell wieder in die horizontale Fluglage zurück,egal in welcher Fluglage sich das Modell bis zu diesem Zeitpunkt befindet.Angle of inclination of the model in relation to the optical horizon. The autopilot can be used with any remote control system that has a positive control pulse with positive polarity. The autopilot can be switched on or off using the remote control that is also used to control the model aircraft. When switched on, the autopilot signals are overridden by the signals from the remote control. If the pilot lets go of all the control levers on his remote control, the optical flight attitude controller brings the model aircraft back to the horizontal flight attitude, regardless of the flight attitude the model was in up to that point.

Claims (1)

SchutzanspruchsProtection claim l)Optischer Autopilot zur automatischen Fluglageregelung von Modellflugzeugen. Bestehend aus einer Steuerelektronik(l) und einem optischen Differentialgeber (J2") , verbunden durch zwei 3-adrige Kabel mit Steckern. Dadurch gekennzeichnet, daß der optische Differentialgeber(2) außen unten am Rumpf des Modellflugzeuges angebracht werden muß (Skizze 2).l)Optical autopilot for automatic flight attitude control of model aircraft. Consisting of control electronics (l) and an optical differential sensor (J2"), connected by two 3-core cables with plugs. Characterized in that the optical differential sensor (2) must be attached to the outside bottom of the fuselage of the model aircraft (sketch 2).
DE29500702U 1995-01-18 1995-01-18 Optical autopilot Expired - Lifetime DE29500702U1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE29500702U DE29500702U1 (en) 1995-01-18 1995-01-18 Optical autopilot

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE29500702U DE29500702U1 (en) 1995-01-18 1995-01-18 Optical autopilot

Publications (1)

Publication Number Publication Date
DE29500702U1 true DE29500702U1 (en) 1995-03-02

Family

ID=8002616

Family Applications (1)

Application Number Title Priority Date Filing Date
DE29500702U Expired - Lifetime DE29500702U1 (en) 1995-01-18 1995-01-18 Optical autopilot

Country Status (1)

Country Link
DE (1) DE29500702U1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001087446A1 (en) * 2000-05-18 2001-11-22 Philippe Louvel Electrical remote-control and remote-power flying saucer

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2001087446A1 (en) * 2000-05-18 2001-11-22 Philippe Louvel Electrical remote-control and remote-power flying saucer
FR2809026A1 (en) * 2000-05-18 2001-11-23 Philippe Louvel Electric toy e.g. flying saucer has remote-control and is powered by an electric motor

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Legal Events

Date Code Title Description
R207 Utility model specification

Effective date: 19950413

R120 Application withdrawn or ip right abandoned

Effective date: 19950601