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Platform/Subsystem Common Interface Control Document Format

AS-1C Avionic Subsystems Committee
  • Aerospace Standard
  • AS5658A
  • Current
Published 2016-05-11 by SAE International in United States
This SAE Aerospace Standard (AS) defines the editorial format and policies necessary for the publication of platform/subsystem Interface Control documents. The Common Interface Control Document Format Standard defines a common format for platform to subsystem interface documents to facilitate subsystem integration. This aerospace standard specifies the common technical data sections for the Common Interface Control Document Format down to the third header level for the majority of sub-sections. The Common Interface Control Document Format Aerospace Standard provides a structured document format in appendixes supported by example paragraphs, drawings, etc.
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Requirements Document for Sensor/Video Interconnect Subsystems with Rationale

AS-1C Avionic Subsystems Committee
  • Aerospace Standard
  • AIR4911
  • Current
Published 2013-09-19 by SAE International in United States
The purpose of this document is to establish the requirements for sensor/video interconnect subsystems. These requirements have been driven predominantly, but not exclusively, by aerospace-type military platforms and commercial aircraft. These requirements are intended to be used as the criteria to establish a sensor/video interconnection standard that will foster the development of common hardware to simplify the total interconnectivity of future avionics platforms.
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Installation and Test of Electronic Equipment in Aircraft General Specification for

AS-1C Avionic Subsystems Committee
  • Aerospace Standard
  • AS8700A
  • Current
Published 2013-09-13 by SAE International in United States
This specification covers the general requirements for the installation and test of electronic equipment in piloted aircraft.
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AS6169: Interface Standard, Airborne EO/IR Systems, Mechanical

AS-1C Avionic Subsystems Committee
  • Aerospace Standard
  • AS6169
  • Current
Published 2013-02-14 by SAE International in United States
This standard defines the mechanical interface and specifies provisions for the electrical and environmental connectors between the host aircraft (“platform”) and a turreted electro-optic/infrared (EO/IR) sensor.
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Interface Standard, Airborne EO/IR Systems, Maintenance and Test

AS-1C Avionic Subsystems Committee
  • Aerospace Standard
  • AS6165
  • Current
Published 2012-12-05 by SAE International in United States
This standard defines the use of data interfaces between a host platform and an electro-optic/infrared (EO/IR) system for maintenance and test (M&T) purposes. In particular, this standard defines the use of the data interfaces in order to facilitate the: a confirmation of system performance and function; b external initiation of built-in-test (BIT) functions; c performance of other diagnostic tests of system health; d downloading M&T data; e uploading software changes. This standard does not cover mechanical or electrical interfaces, nor does it define the basic platform-to-sensor communication protocols and formats. Furthermore, this standard does not address software changes that are made by the manufacturer and not accessible at the sensor interfaces. Data protocols and formats are covered by AS6135. Electrical interfaces are covered by AS6129. This standard covers the use of the interfaces defined by AS6129 and AS6135 for the purposes described herein.
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Interface Standard, Airborne EO/IR Systems, Data

AS-1C Avionic Subsystems Committee
  • Aerospace Standard
  • AS6135
  • Current
Published 2012-12-05 by SAE International in United States
This standard defines the data interfaces between a host aircraft (“platform”) and an Electro-Optic/Infrared (EO/IR) sensor. These data interfaces cover various types of data including: imagery, metadata, command, status, and responses (CSR), geospatial postion, time, test and maintenance, and hand-controller. This standard does not cover mechanical or electrical interfaces.
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AS6129: Interface Standard, Airborne EO/IR Systems, Electrical

AS-1C Avionic Subsystems Committee
  • Aerospace Standard
  • AS6129
  • Current
Published 2012-12-05 by SAE International in United States
This standard defines a generic set of electrical interfaces between a host aircraft (“platform”) and an electro-optic/infrared (EO/IR) sensor. This includes connectors, cabling, fiber optics, signals, and power.
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Platform/Subsystem Common Interface Control Document Format

AS-1C Avionic Subsystems Committee
  • Aerospace Standard
  • AS5658
  • Historical
Published 2009-02-13 by SAE International in United States
This SAE Aerospace Standard (AS) defines the editorial format and policies necessary for the publication of platform/subsystem Interface Control documents. The Common Interface Control Document Format Standard defines a common format for platform to subsystem interface documents to facilitate subsystem integration. This aerospace standard specifies the common technical data sections for the Common Interface Control Document Format down to the third header level for the majority of sub-sections. The Common Interface Control Document Format Aerospace Standard provides a structured document format in appendixes supported by example paragraphs, drawings, etc.
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IEEE-1394b Interface Requirements for Military and Aerospace Vehicle Applications

AS-1C Avionic Subsystems Committee
  • Aerospace Standard
  • AS5643
  • Historical
Published 2004-12-30 by SAE International in United States
This SAE Aerospace Standard (AS) establishes the requirements for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. It defines the concept of operations and information flow on the network. As discussed in 1.4, this specification contains extensions/restrictions to “off-the-shelf” IEEE-1394 standards, and assumes that the reader already has a working knowledge of IEEE-1394. This document is referred to as the “base” specification, containing the generic requirements that specify data bus characteristics, data formats and node operation. It is important to note that this specification is not stand-alone - several requirements provide only example implementations and delegate the actual implementation to be specified by the network architect/integrator for a particular vehicle application. This information is typically contained in a “network profile” slash sheet that is subservient to this base specification. In a similar manner, the electrical characteristics of the bus media, as well as connector information is contained in a “physical layer” slash sheet, that also may be unique to a particular vehicle application. In summary, full understanding of this…
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Installation and Test of Electronic Equipment in Aircraft, General Specification For

AS-1C Avionic Subsystems Committee
  • Aerospace Standard
  • AS8700
  • Historical
Published 1999-07-01 by SAE International in United States
This specification covers the general requirements for the installation and test of electronic equipment in piloted aircraft.