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ISHM for Exploration Mission Systems Carlos Garcia-Galan SIcon 2005 February 8, 2005

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Page 1: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

ISHM for Exploration Mission Systems

Carlos Garcia-GalanSIcon 2005

February 8, 2005

Page 2: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

2SIcon 2005

Systems of Systems Approach

Page 3: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

3SIcon 2005

The C&W Outlook today

Page 4: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

4SIcon 2005

Autonomy Requirements for Space Exploration

ShuttleISS

CEV

Moon Missions

Mars and Beyond

ISHM is a key enabler for automating space flight operations

ApolloMercury/Gemini

Vehi

cle

Au t

ono m

y N

eeds

1960 1980 2000 2020 2040

Page 5: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

Building a Sustainable Space Exploration Program

5SIcon 2005

• Reliable/Safe- Robust and Fault Tolerant systems- Crew and vehicle safety and mission success- Increased spacecraft and crew autonomy

Reduced dependency in critical, real-time Mission Control supportReduced time to execution of failure mitigation actions

- Intelligent Fault Detection and Response for localized subsystem failures or system-wide anomalies.

- Launch Vehicle early anomaly detection

• Effective- Enhanced Subsystem efficiency/margins- Data-Rich Systems

• Affordable- Increased spacecraft and crew autonomy

Reduced Mission Control manning requirementsReduced Astronaut and Operator Training Requirements

- Innovative Reduced Ground manning concepts- Enhanced system margins

• Flexible and expandable- Abundant software re-use and missionization- Increased network information availability- On-board mission planning capability

Flexible mission plans

Safe system and human integration

Page 6: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

6SIcon 2005

Automated Mission Management Systems

EPSHW

TCSHW

ECLSSHW

GNCHW

C&DHHW

…HW

InstrumentationSmart sensors

Wireless TechnologyStructural sensing

Instrumentation modeling/optimal sensor placing

Intelligent Mission Mgt Framework

Sub-SystemsSubsystem Health Mgt

Fault Detection AlgorithmsStructural Health Mgt

RAD-Hard avionicsAdvance/Reconfigurable communications

ISHM Mission PlanTask Automation

HCI

Page 7: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

7SIcon 2005

System Health State Stakeholders

ISHM system provides the Health State information

needed for both human and automated decisions

Logistics Systems

Mission Planning & Scheduling

Systems

Vehicle Management

Systems

Ground Operations

System Health StateRoot Cause Failures

Impacts of FailurePrecursors to Failures

Abnormal Wear and Degradation

Informed Mission

Operations Teams

Procedure Management

Systems

Informed Flight Crew

Critical To

Flight Crews

Ground Teams

Automated Syst

ems

Page 8: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

8SIcon 2005

Health Management Processes• Health Management is an expert-intensive process

- Large Mission Control Center- Labor-intensive ground operations- Intensive training of flight crew and mission support teams

• Goals of ISHM Systems- to detect and understand critical failures early enough to

respond and avoid the most serious consequences- to reduce the activity required of Mission Control Center- to reduce the vehicle house-keeping by flight crews- to reduce the amount of training- to streamline the ground processing

• ISHM systems enable more efficient decision processes- Reduce dependency on Earth-based teams- response to malfunctions- mitigating the impacts of failures on the mission- planning and scheduling systems- efficient ground operations

Page 9: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

9SIcon 2005

Health State in Operations

Intelligent C&W

Procedure Management

Situationally Aware Crews Focused on Mission

ExecutionHealth State Information

Strategic Support

Prognostics

Informed Flight Support Team Helping the Crew

Early Event Detection

Informed MaintenanceInformed Launch and Maintenance Teams Deliver a Nominal Spacecraft to Orbit Procedure Database

Plans & Schedules

Autonomous vehicles collaborate with

humans

Page 10: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

10SIcon 2005

Health Management Technology – spiral 1

• Intelligent C&W• Flight-critical failure detection and annunciation• Fast real-time detection and diagnosis• Deterministic diagnosis• Probabilistic analysis and prognosis• Updatable and reconfigurable detection, diagnosis

and prognosis• System of systems architectures to manage health

consistently across the program

System Health State information is vital for keeping the crews safe and programs affordable as the US reaches for sustainable, long-term exploration of space

Page 11: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

11SIcon 2005

Health State for Space Exploration

• Based on the stakeholders’ needs• Take advantage of technological advances• Balance technology with human skills• Establish clear goals for

- More efficient operations- Higher quality of information

Health management in the right amount is required to meet program safety and efficiency needs for sustaining space exploration

Page 12: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

Programs &

Demonstrations

Page 13: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

13SIcon 2005

Honeywell’s Health Management Heritage

FLIGHT• Fully Integrated Solution• Supports safety-critical partitioning• Central Maintenance function• Aircraft Condition Monitoring function• Standard interface to Member Systems• Maintenance tool set provided• Caution and Warning function• Scalable Architecture• Maintenance Integrator role for aircraft

GROUND• Aircraft Maintenance & Operations

Support System (AMOSS)• Integrated Maintenance & Operations• Aircraft/Ground datalink supported

SYSTEM• Primus Epic® 2000+

GROUND• Aircraft Maintenance & Operations Support

System (AMOSS)• Integrated Maintenance & Operations• Aircraft/Ground datalink supported

SYSTEMS• Aircraft Information Management (AIMS) 1990+• Versatile Integrated Avionics (VIA) 1995+

FLIGHT• Fully Integrated Solution• Supports safety-critical partitioning• Central Maintenance function• Aircraft Condition Monitoring

function• Standard interface to Member

Systems• Maintenance tool set provided

Page 14: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

14SIcon 2005

Honeywell’s Health Management Progress

FLIGHT• Heterogeneous, open architecture• Integrated into the avionics• COTS components, development tools• Supports safety-critical partitioning

GROUND• Fully integrated Maintenance & Operations• Seamless integration with Flight system• Spans entire RLV enterprise• COTS foundation (infrastructure)

TECHNOLOGIES• Model-based diagnostics & prognostics• Fault consolidation & root cause• Handles temporal effects on data• Ground-based using telemetry• Integrated procedure management

ISS DEMONSTRATIONS • Mission Control Center (MCC) based• Diagnosis of Electrical, Thermal and

C&DH failures• Depressurization scenarios• Power balance scenarios

Page 15: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

15SIcon 2005

C&CC&CMDMMDM

C&CC&CMDMMDM

C&CC&CMDMMDM

INTINTMDMMDM

INTINTMDMMDM

PMCUPMCUMDMMDMPMCUPMCUMDMMDM

To Downlink

1.1. DDCU Element Temp SensorDDCU Element Temp Sensor

2.2. DDCU Power Supply Temp SensorDDCU Power Supply Temp Sensor

3.3. DDCU DDCU BaseplateBaseplate Temp SensorTemp Sensor

4.4. RFCA Temp Tracking Sensor(Test)RFCA Temp Tracking Sensor(Test)

ElectricalElectricalPowerPowerLoadsLoadsIDAIDA

DDCUDDCURPCMRPCM

RPCMRPCMRPCMRPCM

RPCMRPCM

RPCMRPCMRPCMRPCM

RPCMRPCMRPCMRPCM

AABB

CCDD

EEFF

GGHH

Primary Power

Data Bus

Secondary Power

RFCARFCA

Aft Coolant Loop Payload RackCoolant Loop

RPCMRPCMRPCMRPCM

RPCMRPCMRPCMRPCM

RPCMRPCMRPCMRPCM

RPCMRPCMRPCMRPCM

AABB

CCDD

EEFF

GGHH

ElectricalElectricalPowerPowerLoadsLoads

RFCARFCA

Vehicle-level Modeling

Page 16: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

16SIcon 2005

Diagnosis and Mitigation

Subsytem CSensors “n”

Subsytem BSensors “B”

Subsytem ASensors “A” “A” Sensors

C&W-----------------Root Cause A-----------------

Effect BEffect C

IVHM Diagnostics

“B” Sensors

“C” Sensors

“A” FDIR

“B” FDIR

“C” FDIR

OperatorOperatorC&W

Current

ODFODF

Actions

ODFODF

ActionsAutomated Actions

Automated System Control

Page 17: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

17SIcon 2005

Significance

• Root-cause diagnostics- accomplished using existing sensor and C&W messages- fits well with current sensors, procedures and protocols- significant time in both training for and handling actual

malfunctions can be saved for controllers and crew

• Procedure management- select existing procedure based on diagnostic results

• Prognostic applications- Prognostic/projective techniques can be applied to complex

situations to improve situational awareness

• Technical challenges addressed- loss of comm (including spurious and erratic data)- temporal effects (multi-rate telemetry)

Page 18: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

18SIcon 2005

ISHM Activity ModelActivities are performed to identify, mitigate and resolve system faults...

• Health State DeterminationMonitor, detect, and isolate faults to identify root-cause failures with diagnostics and prognostics

• MitigationAssess impact of failures and mitigateto minimize impact to mission.

• RepairPerform activities to repair failed component and return system to nominal state.

• VerificationPerform activities to verify that repair effectively returns system to nominal state.

Repair Mitigation

Verification Health StateDetermination

InterventionIntervention

Inte

rven

tion

Inte

rven

tion

Automation

AutomationAutom

ation

Autom

ation

ISHMSystem

Page 19: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

19SIcon 2005

Honeywell ISHM Technology

• We’ve done- Diagnostics- Prognostics- Integration with

maintenance systems• It’s needed for

- Flight crew information- Ground crew information- Automation decisions- Improved vehicle

turnaround efficiency• We’re working on

- Procedure management- Impact analysis- Decision support systems- Interface to mission

planners/schedulers

Repair Mitigation

VerificationHealth StateDetermination

ISHMSystem

Diagnostics

Prognostics

Procedure Mgmt

Impact Analysis

Decision Support

Command AutomationIETM

Repair Certification

Autonomous Mission Planners

Page 20: ISHM for Exploration Mission SystemsBuilding a Sustainable Space Exploration Program 5 SIcon 2005 • Reliable/Safe-Robust and Fault Tolerant systems-Crew and vehicle safety and mission

www.honeywell.com