DE690637C - Process for generating a straight glide path for blind landing of aircraft - Google Patents

Process for generating a straight glide path for blind landing of aircraft

Info

Publication number
DE690637C
DE690637C DE1938D0077560 DED0077560D DE690637C DE 690637 C DE690637 C DE 690637C DE 1938D0077560 DE1938D0077560 DE 1938D0077560 DE D0077560 D DED0077560 D DE D0077560D DE 690637 C DE690637 C DE 690637C
Authority
DE
Germany
Prior art keywords
glide path
aircraft
generating
blind landing
straight
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
Application number
DE1938D0077560
Other languages
German (de)
Inventor
Dr-Ing Paul Freiherr Vo Handel
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.)
Deutsche Versuchsanstalt fuer Luftfahrt eV
Original Assignee
Deutsche Versuchsanstalt fuer Luftfahrt eV
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
Priority claimed from DE1937D0076778 external-priority patent/DE687316C/en
Application filed by Deutsche Versuchsanstalt fuer Luftfahrt eV filed Critical Deutsche Versuchsanstalt fuer Luftfahrt eV
Priority to DE1938D0077560 priority Critical patent/DE690637C/en
Application granted granted Critical
Publication of DE690637C publication Critical patent/DE690637C/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S1/00Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
    • G01S1/02Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Traffic Control Systems (AREA)

Description

Verfahren zur Erzeugung eines geradlinig @leges für die Blindlandung von Flugzeugen Das Hauptpatent betrifft ein Verfahren und eine Anlage zur Durchführung dieses Verfahrens, mit deren Hilfe die Erzeugung eines elektrischen Gleitweges zur Blindlandung von Flugzeugen möglich ist. Der Verlauf dieses Gleitweges kommt dem Gleitwege bei normalen Landungen mit Sicht sehr nahe und ist deshalb von besonderem Vorteil. Method for generating a straight line for the blind landing of aircraft The main patent relates to a method and a system for carrying out this method, with the aid of which it is possible to generate an electrical glide path for the blind landing of aircraft. The course of this glide path comes very close to the glide path in normal landings with sight and is therefore of particular advantage.

Bei dem im Hauptpatent beschriebenen Lösungsweg werden zur Erzeugung des Gleitweges zwei verschiedenartige Strahlungsk ennlim.en von an zwei verschiedenen Orten aufgestellten Sendern, und zavar eines auf langer und eines auf ultrakurzer Welle arbeitenden Senders, zum Schnitt gebracht: Bei Versuchen zu diesem Verfahren stellte es sich jedoch heraus, daß die Zunahme der Feldstärke des Langwellensenders nicht immer genau dem theoretisch geforderten Verlauf entspricht, welcher durch gegeben ist, wenn x die jeweilige Entfernung des Flugzeuges von UKW-Sender und d der Abstand der Sender ist. Diese Unregelmäßigkeiten rühren von Verschiedenheiten des Reflexionsvermögens des beim Anflug überflogenen Geländes her. Die Folge davon ist, daß der Gleitweg nicht immer die geforderte Geradlinigkeit aufweist, sondern in unerwünschter Weise geweilt ist. Um diese Schwankungen im Mittel auszugleichen, wird gemäß dem vorliegenden Zusatzpatent eine Anordnung vorgesehen, die statt eines Langwellensenders a (vgl. die Abbildung) deren zwei oder drei (b, c) benutzt. Die lange Welle breitet sich dann gleichzeitig über die Wege r, a und 3 aus, und es wird hierdurch im Mittel ein Ausgleich der unregelmäßigen Langwellenausbreitung erreicht, so daß die Feldstärke jetzt angenähert tatsächlich mit zunimmt und der Gleitweg geradlinig geworden ist. Technisch wäre der Gedanke beispielsweise in der Form durchzuführen, daß die drei Sender a, b, c auf benachbarten Frequenzen arbeiten, die innerhalb der Empfängerbandbreite liegen müssen und Frequenzunterschiede haben, die oberhalb des ausgenutzten Hörbereiches liegen.In the approach described in the main patent, two different radiation characteristics of transmitters set up at two different locations, and one transmitter working on a long and one on an ultra-short wave, are brought to an intersection to generate the glide path However, out that the increase in the field strength of the long-wave transmitter does not always exactly correspond to the theoretically required course, which by is given if x is the respective distance of the aircraft from the VHF transmitter and d is the distance of the transmitter. These irregularities result from differences in the reflectivity of the terrain overflown during the approach. The consequence of this is that the glide path does not always have the required straightness, but is wavered in an undesirable manner. In order to compensate for these fluctuations on average, an arrangement is provided according to the present additional patent which uses two or three (b, c) instead of one long-wave transmitter a (see the figure). The long wave then propagates simultaneously over the paths r, a and 3, and this balances the irregular long wave propagation on average, so that the field strength now actually approximates increases and the glide path has become straight. Technically, the idea would be carried out, for example, in the form that the three transmitters a, b, c work on adjacent frequencies that must be within the receiver bandwidth and have frequency differences that are above the listening area used.

Claims (1)

PATrX T a', SPRL; cfi Verfahren zur Erzeugung eines geradlinigen .Gleitweges für die Blindlandung von Flugzeugen nach Hauptpatcnt 687 3 16, dadurch gekennzeichnet, daß die Langwellenstrahlung mit zwei oder mehreren Sendern erzeugt wird, welche mit Bezug auf die Landebahn derart aufgestellt sind, daß unerwünschte Bodeneinflüsse auf die Strahlung ausgeglichen werden.PATrX Ta ', SPRL; cfi method for generating a straight .Gleitweges for the blind landing of aircraft according to main patent 687 3 1 6, characterized in that the long-wave radiation is generated with two or more transmitters which are set up with respect to the runway in such a way that undesirable ground influences on the radiation be balanced.
DE1938D0077560 1937-12-05 1938-03-20 Process for generating a straight glide path for blind landing of aircraft Expired DE690637C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE1938D0077560 DE690637C (en) 1937-12-05 1938-03-20 Process for generating a straight glide path for blind landing of aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE1937D0076778 DE687316C (en) 1937-12-05 1937-12-05 Process for generating a straight glide path for blind landing of aircraft
DE1938D0077560 DE690637C (en) 1937-12-05 1938-03-20 Process for generating a straight glide path for blind landing of aircraft

Publications (1)

Publication Number Publication Date
DE690637C true DE690637C (en) 1940-05-03

Family

ID=25972769

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1938D0077560 Expired DE690637C (en) 1937-12-05 1938-03-20 Process for generating a straight glide path for blind landing of aircraft

Country Status (1)

Country Link
DE (1) DE690637C (en)

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