NDLI: High performance 1553: a feasibility study

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[1993 Proceedings] AIAA/IEEE Digital Avionics Systems Conference

24th Digital Avionics Systems Conference

The 23rd Digital Avionics Systems Conference (IEEE Cat. No.04CH37576)

Volume 2 - 2004

The 23rd Digital Avionics Systems Conference (IEEE Cat. No.04CH37576)

Track descriptions (Volume 2)

Reducing cost of high integrity systems through model-based testing

Flight computer software testing - [Not available for publication]

Adding natural relationships to Simulink models to improve automated model-based testing

Next generation testing technique for embedded software: abstract semantics analysis

Effects of shilding on interference pathloss related to wireless technology onboard commercial airlines - [Not available for publication]

The role of formal methods in hardware design assurance - [Not available for publication]

Closed-loop neutron particle effects testing on a recoverable flight control computer

Development of expert system for the design of airborne equipment

Fault detection: the effect of unknown distribution of residuals

Maintaining consistency among distributed control nodes

Model-based development for time-triggered architectures

The real Byzantine Generals

Three large LCD cockpit concept for retrofit applications

Statistical and adaptive approach for verification of a neural-based flight control system

A new flight guidance approach based on differential flatness

Development of a fault tolerant flight control system

Auto-coding/auto-proving flight control software

Neuro-fuzzy based controller for landing phase of an aircraft - [Not available for publication]

Track 6 - Flight critical systems

Track 7 - Avionics upgrades and vehicle health management systems

Considerations for upgrading aging military avionics systems with state-of-the-art technology

Operational solutions and technology for mitigating the effects of PED EMI on flight crew displays and systems

Aging avionics and net-centric operations

High performance 1553: a feasibility study

Aircraft health monitoring for maintenance management - [Not available for publication]

Neural network aided adaptive federal kalman filtering for intelligent integrated navigation application - [Not available for publication]

SINS/GPS/TAN/SAR integrated navigation system based on adaptive federal filtering - [Not available for publication]

Integration of communication and computational architectures for HUMS

Reusability: a technique for the design of HUMS architectures

Reconfiguring HUMS architectures for changing environments

Multivariate fault detection with convex hull

A unified system to provide crew alerting, electronic checklists and maintenance using IVHM

Prognostics and health management for improved dispatchability of integrated modular avionics equipped aircraft

Track 8 - Open systems architecture

Next generation COTS-commercial IP blocks in avionics

Safe COTS graphics solutions: impact of DO-254 on the use of COTS graphics devices for avionics

A system level view of avionics/vetronics cooling options for harsh environment two-level maintenance systems - [Not available for publication]

Implicit intent information for conflict detection and alerting

An open software architecture for high-integrity and high-availability avionics

Open avionics systems development utilizing the time tiggered protocol - [Not available for publication]

Topic paper on distributed power on small platforms - does it make sense? - [Not available for publication]

The application of fiber optic wavelength division multiplexing in RF avionics

Distributed control system for fuel management using CANbus

The concept of remote maintenance monitoring and its computer architecture

Design of airborne encoder decoder using powerpc - [Not available for publication]

Airplane data networks and security issues

Security architecture for aeronautical networks

Transforming avionics architectures to support network centric warfare

High assurance security and safety for digital avionics

Track 9 - Systems engineering

Third-party tools enable NAS modernization planning

How to deliver quality on time - [Not available for publication]

Prototyping interactive cockpit applications

Task sequencing for optimizing the computation cycle in a timed computation model

Madrid airport: a new integration design for a new operational model

High speed fiber optic transceivers with built-in test capability

Time-triggered communication for distributed control applications in a timed computational model

Avionics fiber-optic and photonics network preliminary technology readiness assessment

Methods of implementing very high performance avionics processing circuits using FPGAS - [Not available for publication]

21st century challenge: thermal management design requirements

Mission level design of avionics

Distributed collaborative environments for systems engineering

UWB EMI to aircraft radios: field evaluation on operational commercial transport airplanes

Track 10 - Software engineering

TDMS: test data management system for aviation software

Strategy for inter-model connectivity (SIM-C)

Task design and verification testing for certification of avionics equipment

A FPGA based real-time analyzer for in-flight software & system testing - [Not available for publication]

Credit determination for flow control in FC-AL

Next generation testing tecrnique for embedded software: abstract semantics analysis

Porting applications to an ARINC 653 compliant IMA platform using Vxworks as an example

Issues on software testing for safety-critical real-time automation systems

Automated airborne flight alert system - [Not available for publication]

Distributed reconfigurable avionics architectures

Anytime scheduling for real-time embedded control applications

The augmented flight deck model (AFDM)

Technical challenges in using object oriented technology in aviation applications

Building and comparing models of user interfaces for air traffic control

IEEE scan-like interface for air traffic control software testing

Track 11 - Communications, navigation, surveillance (CNS) networks

Aviation communications emulation testbed

An optimization for packet delivery in integrated avionics systems

Efficient data storage mechanisms for DAP

Evaluation of services for IPv6 aviation networks

Transport of flight critical data over IP - [Not available for publication]

A data communications concept for a SATS scenario

IEIST force template technology provides a key capability for connecting tactical platforms to the global information grid

Designing adaptive architectures for transoceanic in flight communications

Next generation FANS over Inmarsat broadband global area network (BGAN)

IP connectivity and DAP

Extension on characterizing packet interference in a high-density traffic environment

Mobile IP communications for aeronautical applications

Modeling and simulation of ATS air-ground communications using TCP/IP - [Not available for publication]

TCP splitting protocol for broadband aeronautical satellite network

IMT2000 3G terrestrial standards with applications to airport and terminal air traffic communications

VHDL implementation of a bidirectional interface for 3ATI avionic sub-systems

Total information sharing for pilot situational awareness enhanced by intelligent systems

System-wide information management for aeronautical communications

Extension of a real time simulator to provide live displays, voice over IP and CPDLC for a global CNS system - [Not available for publication]

Advancing air traffic management-FAA'S global communications, navigation and surveillance program (GCNSS) - [Not available for publication]

System wide information management using service oriented architectures for collaborative arrival management - [Not available for publication]

Track 12 - Unmanned vehicle (UAV) systems

Remotely piloted vehicles in civil airspace: requirements and analysis methods for the traffic alert and collision avoidance system (TCAS) and see-and-avoid systems

Obstacle awareness and collision avoidance radar sensor system for low-altitude flying smart UAV

Antenna design of collision avoidance radar system for the smart UAV

Development and evaluation of level 3 situation awareness support functions for a UAV operator station

Obstacle avoidance method in the chaotic robot

Obstacle avoidance methods in the chaotic UAV

Target searching method in the chaotic mobile robot

Target searching method in the chaotic UAV

Trajectories characterization of an autonomous aerial vehicle with a small angle of attack

Automatic positioning of UAVs to optimize TDOA geolocation performance

Approach for autonomous control of unmanned aerial vehicle using intelligent agents for knowledge creation

The Stanford testbed of autonomous rotorcraft for multi agent control (STARMAC)

Development and implementation of new nonlinear control concepts for a UA

Sub-optimal trajectory planning for autonomous navigation of an airship - [Not available for publication]

Track 13 - Space systems

The integration and performance of Honeywell's SIGI navigator with Orbital's Pegasus launch vehicle

Space shuttle UHF communications performance evaluation

A high resolution, integrated data acquisition system for aerospace applications

Next generation space avionics: a highly reliable layered system implementation

Designing a filter adaptation scheme for nozzle load resonance in a thrust vector control system - [Not available for publication]

Volume 1 - 2004

Digital Avionics Systems Conference, 2003. DASC '03. The 22nd

Proceedings. The 21st Digital Avionics Systems Conference

20th DASC. 20th Digital Avionics Systems Conference (Cat. No.01CH37219)

19th DASC. 19th Digital Avionics Systems Conference. Proceedings (Cat. No.00CH37126)

Gateway to the New Millennium. 18th Digital Avionics Systems Conference. Proceedings (Cat. No.99CH37033)

17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)

16th DASC. AIAA/IEEE Digital Avionics Systems Conference. Reflections to the Future. Proceedings

15th DASC. AIAA/IEEE Digital Avionics Systems Conference

Proceedings of 14th Digital Avionics Systems Conference

AIAA/IEEE Digital Avionics Systems Conference. 13th DASC

[1992] Proceedings IEEE/AIAA 11th Digital Avionics Systems Conference

IEEE/AIAA 10th Digital Avionics Systems Conference

9th IEEE/AIAA/NASA Conference on Digital Avionics Systems

High performance 1553: a feasibility study

Content Provider	IEEE Xplore Digital Library
Author	Hegarty, M.G.
Copyright Year	2004
Description	Author affiliation: Data Device Corp., Bohemia, NY, USA (Hegarty, M.G.)
Abstract	MIL-STD-1553's one megabit-per-second data rate is adequate for the vast majority of command and control applications within avionics systems but there are emerging systems that require higher data rates. Implementing higher data rate communication generally requires the use of high speed cables. Installing new cabling in legacy aircraft can be cost prohibitive. This work explores the possibility of extending the bandwidth of MIL-STD-1553 by implementing a broadband communication system over legacy 1553 cabling. Various measurement techniques were employed by Data Device Corporation to characterize the performance of a typical 1553 network and each of its major elements. The results of these measurements are used to predict the theoretical capacity of the network using Shannon's equation. The analysis includes characterization of the signal level, noise level, and bandwidth of various channels within a MIL-STD-1553 network. The goal of the research is to quantify the amount of unused capacity within a MIL-STD-1553 system. This work does not present methods of implementing a broadband system but rather provides a framework and initial results for evaluating the feasibility of such a system. The findings presented in This work suggest that there are hundreds of megabits of theoretical capacity available in a MIL-STD-1553 network. The actual achievable data rates would depend on a number of factors including the waveform (or signal coding scheme), and the 1553 bus topology (i.e. bus length, stub length, and number of couplers). The attractiveness of a high performance 1553 system stems from the reuse of legacy cabling and the ability to add new capability to existing platforms without disturbing existing hardware and software.
File Size	538170
File Format	PDF
ISBN	078038539X
DOI	10.1109/DASC.2004.1390751
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2004-10-28
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Aerospace electronics Communication cables Bandwidth Command and control systems Aircraft Costs Broadband communication Communication systems Measurement techniques Equations
Content Type	Text
Resource Type	Article

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