NDLI: Multiprocessor software development for an unmanned research vehicle

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Proceedings of the IEEE 1988 National Aerospace and Electronics Conference

Proceedings of the IEEE 1988 National Aerospace and Electronics Conference: NAECON 1988 (Cat. No.88CH2596-5)

Detection of a gaseous organophosphorus compound using a supported copper + cuprous oxide island film

Generic ASIC design: a sensible methodology for rapid insertion of VHSIC/VLSIC technology

Enabling technologies for achieving avionics modularization

On optimal rank quantization threshold of nonparametric radar detectors

A VHSIC demonstration radar signal processor

Predictive transform modeling

Interception of FH spread-spectrum signals: performance advantages of cycle detectors

Least squares predictive transform modeling

Dual processor VHSIC MIL-STD-1750 A computer module

The SF1 real-time computer

Ferroelectric non-volatile memory

Tactical mapping in combat aircraft

An emulator for ITARS

ITARS robust demonstration system integration

A proposed local area network for next-generation avionic systems

Intelligent IBM-PC compatible boards support a variety of MIL-STD-1553 applications

On high-speed data bus performance analysis

LAVI 1553 B communication system

The ATAMM procedure model for concurrent processing of large grained control and signal processing algorithms

Resource sharing in a complex fault-tolerant system

Real-time operating system for advanced avionics architecture

PAVE PACE: system avionics for the 21st century

Mission/flight systems integration study: a long term electronics planning project

Performance of fiber optic sensors for aircraft applications

The performance of linear fiber optic data buses

A robust fibre optic active star coupler for the SAE linear token-passing multiplex data bus

A generic ground collision avoidance system for tactical aircraft

Applying electro-tactile display technology to fighter aircraft-flying with feeling again

An alternate approach to data fusion

Geometric modeling of flight information for graphical cockpit display

Enhanced navigation and displays from passive terrain referenced avionics

Electronic warfare situation assessment processing requirements for fighter aircraft of the 1990s

Intelligent flight management in threat environments

A smart fusion track initialization scheme using angle only missile launch warning

Multi-sensor targeting and tracking

Integration of active and passive track files from internetted aircraft for enhanced situation awareness

Specification of internal sensor noise to meet SAR motion compensation requirements

CFAR analysis for medium PRF airborne pulse Doppler radars

Intelligent sensor management for beyond visual range air-to-air combat

Fundamental limitations on the performance of navigation systems

Helicopter navigation algorithms for the placement of sonobuoys in an antisubmarine warfare (ASW) environment

Constant gain analysis for discrete tracking filters

Developments in interpretation of the GLONASS navigation satellite

A laser anemometer reference for AIR data calibration

An integrated probe/sensor design for future distributed air data system applications

Low-cost GPS/INS guided stand-off weapon study

UD factorization applied to airborne Kalman-filter-based fusion

Steady-state performance of the decoupled Kalman filter

Passive location and tracking using DOA and TOA measurements of single nonmaneuvering observer

Use of an external cascade Kalman filter to improve the performance of a Global Positioning System (GPS) inertial navigator

Stochastic adaptive tracker based on noise-corrupted space-time measurement process

Kalman filter residual expert system

Design of nonlinear control systems using CONDENS

Development of a workstation for the integrated design and simulation of flight control systems

A computer algorithm for causal spectral factorization

CAD of nonlinear PID controllers for highly nonlinear servo systems

Solutions of the second IEEE benchmark control problem (missile autopilot)

A new method to design intelligent control systems

A reliable expert system for process control system design

Flight control system design using CAEBEL, a CACSD system

Symbolic computing in computer-aided control system analysis and design

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Prediction of vortex interference on a canard controlled missile

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Automatic limiters in Air Force aircraft flight control systems

Eigenstructure selection for longitudinal flying qualities considerations

On deciding display dynamics requirements for flying qualities

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Design and validation of a fault-tolerant distributed clock

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Evaluation of a second generation reconfiguration strategy for aircraft flight control systems subjected to actuator failure/surface damage

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An approach to the FORTRAN-to-Ada code conversion problem

Rapid prototyping: the procedure for software

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An automated approach to designing real time systems

A framework for evaluating software development methods

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Tracking key indicators in multiple software projects in a dynamic environment

The pursuit of accurate source lines of code sizing

Software size estimation techniques

A decision theory framework for software fault correction

A case study in provisions needed in an Ada runtime to support ATF- and LHX-like real-time embedded systems

An Ada language software architecture for distributed simulation system

Controlling large cyclic avionics software systems written in Ada

An automated quality assessor for Ada object-oriented designs

Applicability of Ada tasking for avionics executives

A conceptual discussion for an airborne graphics software support system

On Bezier curves and surfaces

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An interactive graphics editor with integrated data dictionary for IDEF/sub 0/ structured analysis diagrams

Neural networks as a new strategy for computing

Generic voice interface for cockpit application

Human factors analysis of extravehicular servicing of payloads within the space station servicing facility

Situation awareness global assessment technique (SAGAT)

Improving the field of view for the next generation of US Army Black Hawk helicopters

The use of predictive models for the early assessment of crew station design utilities

Computational human factors in human-machine engineering-the Army-NASA aircrew/aircraft integration (A/sup 3/I) program

C-SAINT: a simulation modeling tool customized for workload and information flow analysis

Rules for fighter cockpit automation

Reconfigurable cockpit development

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Automation and dynamic allocation: engineering issues and approaches

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Electronics on the ejection seat

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Development of an oxygen mask integrated arterial oxygen saturation (SaO/sub 2/) monitoring system for pilot protection in advanced fighter aircraft

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Head-up display symbology for unusual attitude recovery

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Architectural analysis of a shared resource digital signal processor

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Potential benefits of embedded training

Intelligent tutoring systems for Air Force applications

Technology's impact on training fidelity

Use of a decision aid model enhancer (DAME) for maintenance training

Target detection simulation by a passive buoy field to protect an aircraft-carrier task force

Cognitive engineering of training systems for simulators

Simulating simulators with computer based training

Adaptive generation of decision functions for classification of digitally modulated signals

Timing considerations with quadrature sampling-quadrature sampling error formula revisited

Predicting ionospheric scintillation for satellite communications

User commanding of the single channel transponder (SCT) space communications package

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Terrain following/terrain avoidance path optimization using the method of steepest descent

Strategic route planning using informed best-first search

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Verification of electronic material properties and characterization of electronic component failures

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Development of an optimization shell using artificial intelligence techniques

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Knowledge engineering for the Adaptive Tactical Navigator

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A cooperative expert system architecture for embedded avionics

Frequency-based model of memory in neural networks

A hybrid AI/game theory approach to aerial combat simulation

Optical neural network for engineering design

REMIS: the distributed data base solution

Automating the weapon system master planning process

Growing an information system using the TASC-EDGE methodology

Supporting diverse logistics analysis through WSMIS

Resolving maintenance aid/data collection paradoxes

RAES: Reliability Advisor Expert System

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Expert system for depot maintenance of the dual miniature inertial navigation system

The need for an Air Force electrostatic discharge control program: a strategic planning approach

Considerations regarding the management of embedded computer system reserves

REMIS man-machine interface

The Air Force Logistics Command Fiber Optics Program: a strategy to systematically introduce the technology

Acceptance test requirements for the procurement of electrostatic discharge (ESD) protective workstations

Air Force Logistics Command's very high speed integrated circuits (VHSIC) insertion program

An overview of the network repair level analysis model (military systems)

Estimating O&S cost uncertainty: an engineering challenge

Life cycle cost-art or science?

The measures of a system-performance, life-cycle cost, system effectiveness, or what?

Logistics testing

The C-17 Program: a model supportability/sustainability

Diagnostics integration-a TAC maintainer's view

USAF Aeronautical Systems Division's model manpower personnel, and training organization-an update

Integrated Electromagnetic System Simulator (IESS)/Logistics Support Utility Analysis (LSUA): a study into new test facilities and support technologies for integrated communication, navigation, identification

The reliability test and evaluation program for the next generation weather radar (NEXRAD) system

Generic Integrated Maintenance Diagnostics (GIMADS): designing weapon systems with the maintainer in mind

Performance analysis for a candidate linear token-passing, high-speed data bus

A system status monitor for the National Aero-Space Plane

Kalman filter design for control surface failure detection and isolation (flight control)

The flight control maintenance diagnostic system

Distributed Ada real-time kernel

A standard for measures to produce reliable software

IEEE software engineering standards-status and perspective

Resource measurement using a closed-loop EEG control system

Loop-closure of the visual-cortical response

A real time frequency analysis methodology for evoked potential loop-closure

Jet engine diagnostics and trending: roadmap for the future

Comparison of instructional system development (ISD) with systems engineering from the training system perspective

A review of microcircuit and hybrid field failures from Air Force avionic equipment

Modular avionics system architecture decision support system

Logistics data integration system (LOGDIS): connecting logisticians to their data

An avionics integrity mechanical analysis

Improved fault detection using a selected grouping of parity equations for advanced flight control systems

A model for technology anticipation

Parallel processor for the simulation of adaptive networks

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Hypersonic vehicle required aerodynamic prediction accuracy

Miniature millimeter wave covert communications system

Multiprocessor software development for an unmanned research vehicle

Content Provider	IEEE Xplore Digital Library
Author	Thompson, D.B.
Copyright Year	1988
Description	Author affiliation: US Air Force Wright-Aeronaut. Labs., Wright-Patterson AFB, OH, USA (Thompson, D.B.)
Abstract	The Control Systems Development Branch of the Air Force Flight Dynamic Laboratory has been utilizing unmanned research vehicles as low-cost flight testbeds for flight control concepts developed in-house. Recently, the limitations of the aircraft and control system used led to the decision to develop a new low-cost research vehicle and complementary multiprocessor avionics/control system architecture. Effective use of the testbed multiprocessor requires that the applications software of the system must be programmable by applications engineers, who may not be experienced in parallel programming and may not have detailed knowledge of the underlying architecture. The author presents the communications protocols and parallel software design methodology used to develop the applications function for the first phase prototype with this requirement in mind.<>
Starting Page	654
Ending Page	659
File Size	457187
Page Count	6
File Format	PDF
DOI	10.1109/NAECON.1988.195075
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	1988-05-23
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Programming Control systems Application software System testing Aerospace control Aerospace electronics Computer architecture Force control Vehicle dynamics Laboratories
Content Type	Text
Resource Type	Article

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