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    STANAG 4586 – Enabling

    Interoperability

    Terry Bandzul

    CDL Systems LtdCalgary, Canada

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    Presentation Overview

    • NATO STANAG 4586 Overview

    • STANAG 4586 Goals

    • Interoperability Concepts

    • STANAG 4586 In Action

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    Current Problems

    • UAV products - “stovepipe” designs

    • Little to no standardization between systems

    • Proprietary telemetry and sensor data

    streams

    • No capability to interoperate

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    • Conceived in 1998 tostandardize UAV ControlSystem (UCS) interfaces tohelp enable UAV

    interoperability

    • NATO Specialist Teamformed from industry andgovernment to develop the

    standard• USN (PMA-263) is

    STANAG 4586 custodian

      STANAG No. 4586

    Edition 1

    NORTH ATLANTIC TREATY ORGANIZATION

    (NATO)

    NATO Standardisation Agency (NSA)

    STANDARDISATION AGREEMENT(STANAG)

    SUBJECT: Standard Interfaces of UAV Control System(UCS) for NATO UAV Interoperability  

    Promulgated on

    Chairman, NSA 

    NATO Project Group 35 (PG/35)

    Background

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    NATO Project Group 35 (PG/35)

    Background

    • Lead efforts to achieve UAV interoperability in Joint,Coalition Operations

    • Lead efforts for UAV Autonomous Operations

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    STANAG 4586

    STANAG 4586 is an Interface Control Definition (ICD)

    STANAG 4586 Defined two new interfaces

    - Data Link Interface, DLI- GCS Air Vehicle interface

    - Command and Control Interface, CCI

    - GCS Command Control Interface

    • Non-existent• Considered essential foundation for interoperable UAV

    systems

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    UAV Interfaces & Standards

    C4I Nodes

    Data Link 

    STANAG 7085

    A i  r   V  e h i  c  l  e  &  P  a  y  l  o a d   C  2  

    P  a  y  l  o a d   D  a t  a 

     Imager y

     D ig i ta l  Messages

    Tactical Messages

    STANAG 5500: ADatP-3

    Payload Data

    STANAG 7023 Primary Imagery

    STANAG 4545 Secondary Imagery

    STANGA 4607 GMTI Radar Data

    STANAG 4609 Motion Imagery

    GroundControl Station

    Focus of 

    STANAG 4586

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    STANAG Key Development

    Principles

    • Data Link Interface (DLI) Messages are air

    vehicle and payload independent – Vehicle/Sensor specific messages are allowed

    • Command and Control Interface (CCI) is

    C4I System/Node independent

     – Leverage existing Standards, e.g. STANAG 5500(USMTF)

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    STANAG 4586

     NATO addressing “technical issues” to enable

    interoperability, these include;

     – DLI and CCI interface definitions

     – Functional architecture definition

     – System, subsystem component identification

    • defines a “common” set of data elementsCommon Data Elements

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    “Common” Data Elements

    Implementation Guide:

     provides the comprehensive description of the

    intention of each message and data element

    in the DLI interface, and makesrecommendations on a common approach

    for implementation –  Removes ambiguity

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    Command & Control

    Interface (CCI)

    • STANAG 4586 provides an interface

     profile that defines the specific choices

    applicable to UAVs within each standard,

    thereby ensuring interoperability.

    GCS

    C4I Nodes

    ADat-P3

    USMTF

    STANAG 4545

    ETC.

    UAV/C4I INTERFACE PROFILE

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    STANAG 4586

    In addition, STANAG 4586:

    • uses standards, existing and developing

     – specifies other standards where possible

     – non-proprietary in nature

     – if shortfalls in standards, request updates. ie;

    CRD, extended CRD

     – not redefining standards• defines relationship between the standards

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    Allied Force Interoperability

    Achieve interoperability

     between NATO allied forces

    Common view of Interoperability

    STANAG focus:

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    Interoperability Ideal

    A UAV overhead a compliant GCS, for whichit has not been “natively” developed, could

     be passed for control to this compliant

    station with the vehicle being safely

    controlled to 100 percent of its requiredcapabilities

    Ideal goal of interoperability

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    Multi Vehicle, Modular

    Networked Operations

    Allows individual addressing of specific Systemcomponents

    - the generic interface anticipates that there will be multiple Vehiclesconnected to multiple CUCSs in a networked or standaloneconfiguration, addressing a shared data link resource, or multiple datalinks

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    Interoperability

    US Army

    Class IV UAV

    US NavyTactical UAV

    United Kingdom

    Watch Keeper

    Italian

    Predator

    • Concept of Operations (CONOPS) and Doctrine “Neutral”

    •Supports evolving CONOPS and Doctrine

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    CONOPS

    Control a single vehicle, of a

    specific type

    What is the advantage to usingSTANAG 4586 ?

    - Sharing the asset

    - considering futureexpandability

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    CONOPS

    Multiple vehicles,

    single type,

    simultaneously

    Multiple Data LinksSingle Common

    Data Link 

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    CONOPS

    Many vehicle types, controlled serially from acommon GCS

    Multiple Data Links

    - One at a time

    Common Data Link - one at a time

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    CONOPS

    Multiple vehicles, multiple

    types simultaneously

    Additional requirements

     – Co-location versus networked

    operation

     – DLI across RF link 

    Multiple Data Links

    Common Data Link 

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    Scalable Interoperability

    • Not always requirement to control 100% of

    vehicle capabilities

     – Expensive undertaking

    • Only control functionality required to be

    interoperable

     – five Levels of Interoperability defined within

    the standard

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    Levels of Interoperability

    • Level I: Indirect receipt/transmission of UAVrelated payload data.

    • Level II: Direct receipt of ISR/other data where“direct” covers reception of the UAV

     payload data by the UCS when it hasdirect communication with the UAV.• Level III: Control and monitoring of the UAV payload

    in addition to direct receipt of ISR/other data.

    • Level IV: Control and monitoring of the UAV,less launch and recovery.

    • Level V: Control and monitoring of the UAV, pluslaunch and recovery functions

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    Modular Control

    Modular Architecture

    - functional separation• situation awareness

    • AV mission execution andmonitoring

    • Payload – monitor, control• Data Links – monitor, control

    Scalable

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    STANAG 4586 In Action

    • VCS-4586, Common User Interface for

    range of controlled vehicles

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    VCS STANAG 4586

    Applications

    • US Army One System

     – RQ-7B Shadow 200 - AAICorp

     – Warrior – GA ASI

    • Barracuda (RIB) – MeggittDefence Systems Canada

    • Grasshopper – Advanced

    Subsonics• Raven – AeroVironment

    • Golden Eye – Auroa

    • Aerosonde - AAI Corp.

    • Grasshopper - AdvancedSubsonics & Xiphos

    • Silver Fox - Advanced Ceramics

    • Scan Eagle - Boeing

    • Kingfisher & Other - BAESystems

    • RTB (Research Test Bed) - CAE /CDL Systems

    • Blade - Ultra

    Grasshopper Shadow 200 Warrior 

    Silverfox

    Scan Eagle

    Kingfisher 

    AerosondeBlade

    Hammerhead

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    Mini UAV to MALE

    • Currently, how is it that the sameCUCS software can be used to controlvehicles as diverse as a mini UAV anda MALE?

    • VSMs are key, but not 100% of theanswer 

    • STANAG 4586 is scalable inimplementation, from a singleoperator, single laptop for a miniUAV, to dual operator workstationsfor MALE UAVs.

    •STANAG 4586 is configurablethrough VSM messages and/or throughconfiguration files

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    VCS-4586

    Common User Interface

    • Configuration Messages are used to request air

    vehicle and payload configuration information.

     – Expected range of vehicle parameters

     – Applicability of generic parameters to vehicle

     – Availability of generic parameters from vehicle

     – Extensibility of parameters

    • The CUCS uses this information to configure thedisplays for the Air Vehicle/ payload.

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    HCI - Configurable Elements

    Message #1201: Display Unit Request

    The CUCS uses the Display Unit Requestmessage to identify the display units that the VSM

    is required to use in Remote Displays.

    Examples:

    • Distance

    • Altitude• Speed

    • Temperature• Mass/Weight

    • Angles• Pressure

    Message #1202: CUCS Resource Report

    Used to communicate to the VSM the resourcesavailable within the CUCS for managing remotedisplays to be presented at the CUCS.

    Examples:

    • JAVA Engine Available

    • PDF Reader Available• X Window Server Available

    • X Window Display Number 

    • X Window Screen Number • Display Window Horizontal Width

    Message #1303: Field Configuration Command

    This message is used by the CUCS to configure

    any GUI components associated with a formattedDLI message field, where the state of the field maybe altered in accordance with the contents of thismessage.

    This message is sent from the VSM to the CUCSwhenever the controllable state of a field or an

    enumeration within a field changes thus identifyingthe allowable states of control at the VSM for thespecified parameter.

    Examples:

    Altitude Command Type

    Heading Command

    Speed Type

    Altitude Type

    Antenna Type

    Flight Mode

    (over 30)

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    Parameter Ranges

    CUCS supports full STANAG parameter ranges,

    But Configures the displays to suit the selected

    vehicle

    Altitude scale

    modified

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    Parameter Applicability

    CUCS must be capable of supporting allgeneric functionality,

     but is expected to remove functionality

    unsupported by the controlled vehicle

    Flight modes

    removed

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    Vehicle Logic

    CUCS can not know the control logic for allvehicles,

    therefore the VSM identifies the current state

    of vehicle parameters

    Mission mode

    unavailable

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    Parameter Extensibility

    Ability to extend generic capabilities with vehiclespecific capabilities, for specific parametersthrough the DLI mechanism,

    for tight integration into a single application

    - for operator ease of use

    - for flight criticality or flight safety

    Added custom Flightmode -> Roll

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    Private Messaging

    Ability to integrate generic capabilities with vehiclespecific capabilities, using privately defined DLImessages,

    to tightly integrate into a single application

    - for operator ease of use

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    Configured Panel

    Compliant

    Configured

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    What Interoperability Means

    • UAV control systems can be developed to meet“national” requirements

    • UAVs for Country A may use one user interface,

    regardless of UAV type; UAV controllers forCountry B could be using a completely differentuser interface, even though they may be operatingthe same UAVs

    • UAV operated by Country A can be handed off toCountry B, even though the ground stations aredissimilar 

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    What Does S4586 Do for Me?

    • Reduces Costs - Capital and O&M• Simplifies C4ISR Systems Integration

    • Reduces Logistics Tail

    • Decouples UAV development from GCS Integration

    • Supports National GCS Development with own

    CONOPS and Training

    • In Coalition Operations, STANAG 4586 Supports

    Multinational Partners Sharing Data from multipleUAVs from multiple countries.

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    Acquisition of UAV Systems

    STANDARDIZED INTERFACE DECOUPLES 

    THE GCS & AIR VEHICLE

    STANAG 4586 StandardGCS/Air Vehicle Interface

    The acquisition of air vehicles can

    occur independent of other elements

    of the UAV system (eg. the GCS).

    The GCS can be sustained, upgraded

    and produced in multiple

    configurations independent of the

    other elements of the system.

    Ground

    Control Station

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    Interoperability Does Not Mean

    • Common User Interface for All Users

     – French Operator does not sit in a German

    shelter 

    • Common Training – Train for your own system

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    Trends Affecting STANAG

    • Bandwidth Reduction – Common Protocol viaRF Link 

    • Trend toward network-centric CONOPS

    - SOA (service-oriented architecture) – provideservices to the network.• Trend toward increasing system autonomy

    - Autonomy messages added to the STANAG 4586,operators become system supervisors

    • Trend toward collaboration among systems- Ship to ship messaging and interactions

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    Conclusions

    • STANAG 4586 Edition 2 is ready.

    • STANAG 4586 is implementable.

    • STANAG 4586 is implemented on several realUAVs.

    • A common User Interface per User is achievable.

    UAV interoperability is now possible.

    Is Interoperability possible?

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    STANAG 4586: Enabling

    Interoperability

    THANK-YOU

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    A NATO UAV System

    GROUND

    CONTROL

    ELEMENT

    C

    C

    I

    AIR VEHICLEELEMENT

    PAYLOAD ELEMENT

    Air DataTerminal

    Payload Data

    Ground DataTerminal

    ExternalC4I

    Systems

    Control

    Status

    AIR COMPONENT

    GROUNDCOMPONENT

    DLITasking

    Status

    DataDissemination

    7085

    7023, 4545,4607, 4609D

     a t   aL i  nk 

    STANAG 4586STANAG 4586

     O     P     E     R     A     T     

     O     R     

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    STANAG 4586 Goals

    • Interoperability amongst Allied Forces

    • Diverse Concepts of Operations

    • Network Centric Operations.

    Secondary considerations:

    • Common ground control station per user vrs Scalability

    • One operator, many vehicles

    • Modular design

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    Interoperability - ONE System

    QuickTime™ and aTIFF (LZW) decompressor 

    are needed to see this picture.

    US Army TUAV Project

    Office has introduced

    “ONE System” to fly:

    • Shadow 200 – (AAI Corp.)

    • Hunter

     – (Northrop Grumman)

    • Sky Warrior

     – (General Atomics - ASI)

    Based on the VCS by CDL Systems Ltd.