flight controls q&a

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Federal Aviation Administration 1 Flight Controls Q&A Presentation to: NASA ODM By: Wes Ryan, Manager ACE-114 Date: March, 2016

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Page 1: Flight Controls Q&A

NASA ODM Workshop Federal AviationAdministration 1January 2012

Flight ControlsQ&A

Presentation to: NASA ODMBy: Wes Ryan, Manager ACE-114Date: March, 2016

Page 2: Flight Controls Q&A

NASA ODM Workshop Federal AviationAdministration 2

Objective• Flight Path Control - Key Enabler for ODM• Summarize FAA Efforts & Next Steps

Page 3: Flight Controls Q&A

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Long Term Goals• Create Regulatory Environment

for Safer, More Innovative Aircraft• Work With Industry, NASA, &

Others to Plan for Future• Consider Role of Flight Path

Control• Technology More

Affordable Every Year

Page 4: Flight Controls Q&A

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FAA R&D Efforts & Planning• The Part 23 Rewrite, FAA R&D, Standards

Work, & UAS Certification Efforts All Fit Together - Prototyping New Ideas

• Creating a Long Term Vision for GA - Start With Low Risk, Work up to Higher Risk

• Our R&D Building Blocks• AOA for Stall Prevention• Dual Axis “Smart” Autopilots• Non-Deterministic & Adaptive Systems

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Identify Building Blocks• Started with Sensors – AHRS,

AOA, etc. • Better Sensors, Design

Tools, Actuators, Displays, etc.

• Evolving from Passive/Sensing, to Active Systems, to Adaptive Systems

• Augmented Flight Path Control - FBW

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Why AOA Sensors?• Non-required system• Provides Direct Indication of Stall • Pilots Trained on Speed, but

Dynamic Stall is Common – Better Information

• Low Risk Solution to Root Cause of Accidents in GA

Page 7: Flight Controls Q&A

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“Smart Autopilot” Work• Provide Envelope Protection

• Garmin’s GFC-700, Avidyne DFC-90• How Can we Simplify Certification?

• Real Time Integrity Monitoring?• Independent Monitor with Reversion?• “Black Box” with Executive Monitor on

Behavior of System?• Working with Adaptive Aerospace on

Solutions

Page 8: Flight Controls Q&A

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Retrofit - TruTrak ECO• Tru Trak Designing Separate Surface

Autopilot – Easier Interface for Existing Aircraft

Page 9: Flight Controls Q&A

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• Level 0 – Warning systems alone• Level 1 – multiple automatic control functions (steering,

braking, throttle) that operate independently• Level 2 – Combined function automation, but driver still

responsible for monitoring the road. The driver is expected to be available to assume control on short notice.

• Level 3 – Driver is not expected to be constantly monitoring. However, the driver is available to assume control with sufficiently comfortable transition time

• Level 4 – Full self-driving cars where the vehicle performs all critical driving functions.

Should We Consider NHTSA?

Page 10: Flight Controls Q&A

What Design Best Practices?1. Modular Software

Architecture• Top down architecture hierarchy

with clearly specified interfaces

2. Functionally Partitioned Modules• Each module limited to a single

safety function• Software isolation of Vehicle

performance modeling

3. Computational Agility• Rapid assessment of vehicle

situational hazards with quick and decisive mitigation of those hazards

Page 11: Flight Controls Q&A

How We Will Achieve The Vision?• A Software Framework

• Expandable Variable-Autonomy Architecture (EVAA)

• A Federated Architecture• Safety Systems

• 1• 2• 3…

• Flight Executive• Software Structure &

Techniques

• Classical & Non-Classical Verification Methods

• Demonstration of the Technology

• Flight Demonstrations• Social Interaction EVAA Components

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Integrated Controls

• Seek Whole Aircraft System• Avionics, Propulsion, Flight Path

Management, Configuration Management• Controls Thrust, Aero, Configuration, System• Follows Intended Point to Point Flight Path

• Rely on Safety Net & Mitigations• Safe Degraded Modes – Self Protection• Auto-recovery – Panic Button• Whole Aircraft Parachute

• Considering an ASTM Group to Create Standards

Page 13: Flight Controls Q&A

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Impact on Skill?• Contrasting Technology

• Legacy Instruments – Federated• Modern Device – Intuitive Interface

• Expected Skill – Pilot Flies Through System• Controls “fly” but direct flight path control by

DFCS, not the pilot (“On” the Loop)• Clear System Status and Pilot Expectation• Pilot Pulls the “Rip Cord” – Parachute

Recovery for Catastrophic Failure of System

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Discussion……