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Transcript :
Skies around the world are becoming increasingly crowded. In the U.S., the Federal Aviation Administration estimates that rising numbers of flights and passengers will overwhelm the current air traffic control system by 2015, leading to an increase in delays, higher costs, and greater environmental impact.
To meet this challenge, the FAA is building NextGen, America’s air traffic control system of the future, which will make air travel safer, more efficient, and better for the environment. The backbone of this system is a new technology called Automatic Dependent Surveillance — Broadcast, or ADS-B.
ADS-B enables the widespread use of satellite-based GPS technology in aviation. It provides air traffic controllers and pilots with information that will help aircraft efficiently navigate our increasingly congested airspace.
So how does it work? ADS-B allows planes to determine their exact location using GPS. That information is broadcast to other nearby aircraft and ADS-B ground stations, which relay the information to air traffic controllers. Additionally, a signal with flight, weather, and radar data is broadcast back to the plane.
To make this possible, aircraft will be required to have equipment that continually broadcasts their position, and, optionally, additional equipment that enables the aircraft to receive those messages from other planes, as well as information from ground stations.
This continuous and nearly instantaneous cycle of broadcasts gives air traffic controllers and pilots a complete and more up-to-date picture of their airspace.
ADS-B provides updates 12 times more frequently than radar, which means better coordinated takeoffs and landings, less time sitting on the ground or circling in the air, more direct routes that shorten flight times, and fewer delays.
Increased airspace efficiency is another chief benefit of ADS-B. The technology puts more information in the hands of pilots, who will now have access to air traffic control data on display screens right in the cockpit, while controllers will guide them from displays which will be more accurate than ever before. This extra layer of data enables advanced air traffic control procedures allowing aircraft to fly more closely together with fewer instructions from the ground.
ADS-B also benefits the environment by enabling a more direct approach and a power-saving continuous descent to the runway. For example, an airliner using these procedures during every landing would save enough fuel to reduce its annual carbon emissions by an amount equal to that of more than 100 cars.
ADS-B will have direct effects on local markets. For example, in the Gulf of Mexico, ADS-B stations installed on offshore oil rigs are providing full air traffic control coverage over the Gulf for the first time in history. ADS-B dramatically increases efficiency for both low-altitude helicopter traffic servicing oil rigs and for high-altitude air transport aircraft traversing the Gulf.
Right now, ITT is working with the FAA on a nationwide rollout of ADS-B. ADS-B technology will enable air travel that is safer, more efficient, and better for the environment. This technology, a cornerstone of NextGen, will revolutionize the future of flying. And it’s on its way right now.

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ads-37a-prf, aeronautical design standard – EverySpec

ADS-37A-PRF, AERONAUTICAL DESIGN STANDARD: ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E3) PERFORMANCE AND VERIFICATION REQUIREMENTS (28 MAY 1996)., …

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Source: everyspec.com

Date Published: 4/12/2021

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ADS-37A-PRF – 28 MAY 1996

ADS-37A-PRF. AERONAUTICAL DESIGN STANDARD. ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E³). PERFORMANCE AND VERIFICATION REQUIREMENTS.

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Source: www.avmc.army.mil

Date Published: 10/27/2022

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ADS-37A-PRF:1996 – Normadoc

ADS-37A-PRF:1996 · Electromagnetic Environmental Effects (E3) Performance Verifications Requirements. · Additional Info …

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Source: www.normadoc.com

Date Published: 12/10/2021

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Electromagnetic Environmental Effects System Testing – DTIC

… as well as ADS-37A-PRF Aeronautical Design Standard for the Electromagnetic Environmental Effects E3 Performance and Verification Requirements.

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Source: apps.dtic.mil

Date Published: 12/10/2022

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ADS-37A-PRF ELECTROMAGNETIC ENVIRONMENTAL EFFECTS

ADS-37A-PRF, AERONAUTICAL DESIGN STANDARD: ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E3) PERFORMANCE AND VERIFICATION REQUIREMENTS (28 MAY 1996)

ADS-37A-PRF, AERONAUTICAL DESIGN STANDARD: ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E3) PERFORMANCE AND VERIFICATION REQUIREMENTS (28 MAY 1996)., This document establishes electromagnetic environmental effects (E3)performance and verification requirements for aircraft systems.

ADS-37A-PRF:1996

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Aeronautical Design Standard, United States Army Aviation and Missile Command – Electromagnetic Environmental Effects Performance and Verification Requirements

Lightning Environment (Direct Effects Testing). For design and verification purposes, the natural

lightning environment (which comprises a wide statistical range of current levels, duration, and number of

strokes) is represented by current components A through D, and voltage waveforms A, B, and D as defined

in paragraph 23.5 of RTCA/DO—I6OC. Guidance for application of these waveforms is also given in

Section 23 of RTCA/DO-I6OC.

Lightning Environment (Analysis and Indirect Effects Testing). Appendix III of FAA/AC 20-136

contains idealized mathematical representations of a severe natural lightning environment. Those

waveforms A, B, C, and D are derived from cloud-to-ground lightning discharges. Waveform H represents

the high rate—of-rise effects including those from intracloud and cloud-to-cloud discharges. These idealized

waveforms can be used as the bases for either tests or analyses of the effects of a severe lightning

environment on aircraft electrical/electronic systems. Test waveforms, of necessity, will be only

approximations of the idealized waveforms. Results from test waveforms that deviate from the idealized

waveforms must therefore be analytically relatable to the idealized waveform.

Lightning Attachment Zones. Lightning attachment zones are defined in paragraph 23.2.3 of RTCA/DO—

160C. Guidance for locating the zones on particular air vehicles is discussed in the Section 30.1 of MIL—

STD-1795.

Lightning Effects (Direct and Indirect). The direct effects of lightning are the burning, eroding, blasting,

and structural deformation caused by lightning arc attachment, as well as the high pressure shock waves and

magnetic forces produced by the associated high currents. Direct effects includes the direct coupling of

lightning currents into electrical wiring associated with external lighting, antennas, and other external

equipment. The indirect effects are those resulting from the interaction of the electromagnetic fields

accompanying lightning with electrical/electronic equipment inside the vehicle.

Flight Critical Equipment. E3 generated anomalies involving this equipment would cause immediate or

almost immediate loss of aircraft control or unsafe situations with loss of life a likely occurrence.

Flight Essential Eguipment. E3 generated anomalies involving this equipment could cause an emergency

landing with possible damage to the aircraft, or would cause the pilot to take other emergency action.

Injury or loss of life is possible.

Electromagnetic Environmental Effects System Testing

Accession Number: ADA506300

Title: Electromagnetic Environmental Effects System Testing

Descriptive Note: Final rept.

Corporate Author: ARMY WHITE SANDS TEST CENTER WHITE SANDS MISSILE RANGE NEW MEXICO SURVIVABILITY VULNERABILITY AND ASSESSMENT DIRECTORATE (SVAD)

Report Date: 2009-09-02

Pagination or Media Count: 179.0

Abstract:

This Test Operational Procedure TOP provides the Electromagnetic Environmental Effects E3 interface requirements and verification criteria for airborne, sea, space, and ground systems, including associated ordnance, as stated in military standard MIL-STD-464A Electromagnetic Environmental Effects Requirement for Systems, as well as ADS-37A-PRF Aeronautical Design Standard for the Electromagnetic Environmental Effects E3 Performance and Verification Requirements.

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