WO2014128571A2 - Airborne interactive reconnaissance (acronym air) - Google Patents
Airborne interactive reconnaissance (acronym air) Download PDFInfo
- Publication number
- WO2014128571A2 WO2014128571A2 PCT/IB2014/001310 IB2014001310W WO2014128571A2 WO 2014128571 A2 WO2014128571 A2 WO 2014128571A2 IB 2014001310 W IB2014001310 W IB 2014001310W WO 2014128571 A2 WO2014128571 A2 WO 2014128571A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- aircraft
- vicinity
- air
- mishap
- time
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0004—Transmission of traffic-related information to or from an aircraft
- G08G5/0008—Transmission of traffic-related information to or from an aircraft with other aircraft
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/87—Combinations of radar systems, e.g. primary radar and secondary radar
- G01S13/878—Combination of several spaced transmitters or receivers of known location for determining the position of a transponder or a reflector
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0047—Navigation or guidance aids for a single aircraft
- G08G5/0056—Navigation or guidance aids for a single aircraft in an emergency situation, e.g. hijacking
Definitions
- Open water communication is by high frequency radio on a one to one basis between aircraft and ground stations (air traffic control).
- All aircraft must be equipped with transceivers operating possibly on one dedicated frequency that transmit their call signs at very short intervals and receive and record the call signs or equivalent and GPS data of all other aircraft in the vicinity, against the clock.
- the system may be tailored to operate in send mode with receive/record mode on standby to be triggered by incoming high frequency radio signals from aircraft within reciprocative signal proximity and possibly on board radar used in anti-collision applications. This would utilize recording capacity only when other aircraft signals are receivable, thereby optimizing recording.
- the whole system may well morph into an application derivative as simple as Google "Latitude” in the foreseeable future!
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
Airborne Interactive Reconnaissance (AIR) will use current communication technology with tailored software and switching methodology to communicate all necessary asset recovery data including time, GPS co-ordinates, altitude, call sign etc to operate interactively between Aircraft in flight, in conjunction with, but independent of existing satellite and ground tracking systems. The location of a mishap would then hopefully be recorded on the ancilliary data recorder module of any other aircraft that was in the vicinity at the time. All aircraft in the vicinity of a mishap would be aware of same when alerted. Critical data may be retrieved from any or all aircraft in the vicinity at the time. The data will be available on these aircraft (even without an alert) for the pre-programmed over-record cycle times, after they have landed.
Description
AIRBORNE INTERACTIVE RECONNAISSANCE
Description
Scope
To assist in the location of aircraft in the event of mishap.
Preamble
1) Aircraft enter flight corridors at specific gateways.
2) Flight corridors are relatively well defined in all directions.
3) Ground Radar fades beyond 250Km of Radar station.
4) Open water communication is by high frequency radio on a one to one basis between aircraft and ground stations (air traffic control).
5) Current tracking services are satellite derived (IMARSAT,etc) which are expensive to install, costly to operate and tedious in decoding.
Proposed Method
1) All aircraft have transponders that signal their location to the nearest ground station. This may not be possible over open water.
2) All commercial aircraft fly on designated corridors at cruising altitudes ranging on average from 29,000 to 35,000 ft.
3) Given the density of commercial flights, it should be safe to say that several aircraft will be in relatively close proximity to other aircraft in the air at any given time.
4) The technology to use GSM communications without interference to aircraft navigation and communications is now available and permitted.
5) The use of communication technology (viz locate a lost iPhone anywhere in the world in minutes!) maybe used between aircraft to log ID (call sign), time and GPS coordinates etc. on a hyper-intermittent interactive basis.
6) The record of every aircraft's whereabouts will be logged on the recorders of all other aircraft in the vicinity.
Necessary System Attributes
1 ) All aircraft must be equipped with transceivers operating possibly on one dedicated frequency that transmit their call signs at very short intervals and receive and record the call signs or equivalent and GPS data of all other aircraft in the vicinity, against the clock.
The system may be tailored to operate in send mode with receive/record mode on standby to be triggered by incoming high frequency radio signals from aircraft within reciprocative signal proximity and possibly on board radar used in anti-collision applications. This would utilize recording capacity only when other aircraft signals are receivable, thereby optimizing recording.
The whole system may well morph into an application derivative as simple as Google "Latitude" in the foreseeable future!
2) The duration for which such recordings should be held intact is a practical consideration to be decided viz: a) General alert to aircraft airborne in the vicinity of a suspected mishap. b) Recorder reset times for aircraft on the ground in the absence of an alert (Evidence of a mishap location last recorded). c) Auto over-recording in continuous time cycle capacity of 24 to 36 hours!?
Claims
The Claim
The combination of onboard transponders, transceivers operating possibly on one dedicated frequency and auxi l iary black box recordings on other aircraft in the vicinity should triangu late the location of a m issi ng aircraft more cost effectively and accurately than hithertofore.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/IB2014/001310 WO2014128571A2 (en) | 2014-07-09 | 2014-07-09 | Airborne interactive reconnaissance (acronym air) |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/IB2014/001310 WO2014128571A2 (en) | 2014-07-09 | 2014-07-09 | Airborne interactive reconnaissance (acronym air) |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2014128571A2 true WO2014128571A2 (en) | 2014-08-28 |
WO2014128571A3 WO2014128571A3 (en) | 2015-01-29 |
Family
ID=51391929
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/IB2014/001310 WO2014128571A2 (en) | 2014-07-09 | 2014-07-09 | Airborne interactive reconnaissance (acronym air) |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2014128571A2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018010419A1 (en) * | 2016-07-11 | 2018-01-18 | 吴建钢 | Global positioning function expansion device for black box of aircraft |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110149849A1 (en) * | 1996-12-06 | 2011-06-23 | Edwin Brownrig | Wireless black box communication systems and methods |
US20130317673A1 (en) * | 2010-11-12 | 2013-11-28 | Airbus Operations (Sas) | Method and system of transmitting and receiving data originating from an aircraft black box |
-
2014
- 2014-07-09 WO PCT/IB2014/001310 patent/WO2014128571A2/en active Application Filing
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110149849A1 (en) * | 1996-12-06 | 2011-06-23 | Edwin Brownrig | Wireless black box communication systems and methods |
US20130317673A1 (en) * | 2010-11-12 | 2013-11-28 | Airbus Operations (Sas) | Method and system of transmitting and receiving data originating from an aircraft black box |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018010419A1 (en) * | 2016-07-11 | 2018-01-18 | 吴建钢 | Global positioning function expansion device for black box of aircraft |
Also Published As
Publication number | Publication date |
---|---|
WO2014128571A3 (en) | 2015-01-29 |
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