Title: UAS Propulsion Systems: Gap Analysis Risk Analysis
1UAS Propulsion SystemsGap Analysis / Risk
Analysis
- Christopher Griffis, Timothy Wilson
- March 13, 2008
2Overview
- Project plan and schedule
- Project review up to last meet
- Summary of new efforts
- Description of plan to finish
3UAS Propulsion SystemsGap Analysis / Risk
Analysis
4Project Plan Gap Analysis
5Project Plan Risk Analysis
6Project Plan Wrapping Up
7UAS Propulsion SystemsGap Analysis / Risk
Analysis
8Gap Analysis Mechanism
- Modified spreadsheet to cover the new dimensions
of analysis (coined term Dimensions of
Applicability) - Marshall parameters
- Propulsion system categories from Tech Survey
- Relation to the Conceptual Model
- Color-coded grouping for layering of information
9Spreadsheet Sections vs. Technology and
Conceptual
10Gap Analysis EM Systems
RP Issues that are covered by existing
regulation (very large region)
GT Issues not covered by existing regulation
(very small region)
RP Issues not covered by existing regulation
(very small region)
Regulatory Gaps!!! (Areas not covered, even by
interpretation of existing FARs)
EM Issues Covered by interpretation of FARs for
existing RP/GT Regulation
11UAS Propulsion SystemsGap Analysis / Risk
Analysis
12Gap/Risk Documentation (I)
- Intro
- Project description (objectives, scope)
- Background (tech survey, conceptual model,
foundation for gap and risk analysis) - Gap Analysis
- Discussion of gap analysis artifacts
spreadsheet, legend, Dimensions of Applicability
(DofApropulsion systems affected, Conceptual
Components affected) - Gap Analysis process description
- Setup
- Line-by-line applicability assessment and Global
Evaluation - Gap documentation
- The Gap Analysis
- Global gaps
- Specific gaps
13Gap/Risk Documentation (II)
- Risk Analysis
- Discussion of risk analysis artifacts
- Preliminary hazard list
- Failure modes and effects analysis
- Discussion of risk analysis process
- The Risk Analysis
- Conclusions and Recommendations
- References
- Appendices
14Gap Analysis Objectives (Revised)
- Identify the categories of regulatory guidelines
that will be looked at - Perform proper scoping of the project to make the
findings manageable and usable. - Determine how to manage the complexity of all the
dimensions of this gap analysis - Create a spreadsheet that concisely and compactly
stores and communicates this information - Perform a global assessment of gaps that exist
with regard to the current state of regulation - Perform an individual assessment of each FAR as
it relates to UAS propulsion, explaining its
assessment with regard to the applicability
criteria. - Create a document that encapsulates the essential
information in summarizing and communicating
these gaps
15Risk Analysis Objectives (Revised)
- Based on FAA SRM Order 8040.4
- Implement safety risk management by performing
risk assessment and analysis and using the
results to make decisions - Plan the risk assessment and analysis must be
predetermined, documented in a plan which must
include the criteria for acceptable risk - Hazard identification the hazard analyses and
assessments required in the plan must identify
the safety risks associated with the system or
operations under evaluation - Analysis the risks must be characterized in
terms of severity of consequence and likelihood
of occurrence - Risk Assessment the risk assessment of the
hazards examined must be compared to the
acceptability criteria specified in the plan and
the results provided in a manner and method
easily adapted for decision-making - Decision the risk management decision must
include the safety risk assessment and the risk
assessments may be used to compare and contrast
options
16The Fundamental Gap
- Current regulations
- Implicit assumption that propulsion for manned
aircraft only comes from two types of
powerplant/energy transformers gas turbine
engines and reciprocating piston engines - Almost specifically do not regulate the concept
of a pure electrically driven motor as the
powerplant for an aircraft system. - UAS that use EM based propulsion arent covered
- Also means that predicate technologies in the
conceptual chain aren't covered (ES and ET like
fuel cell, long endurance battery,
ultracapacitors, etc) - RESULT
- Using regulatory provisions for things relating
to heat and thermodynamically based means of
propulsion to guide safety aspects of EM based
systems now become a matter of interpretation (as
it stands) - In some cases for EM, there isn't even a basis
for interpretation in existing guidelines - RECOMMENDATION
- Embrace this concept and develop system
size-invariant safety guidelines (regulations)
addressing the needs of pure EM based systems
17The Open-Set Gap
- Current regulations
- Very specific about turbine and reciprocating
engines - Have a scattered collection of coverage
regulations that say, if this cant be done, at
least do this. (tantamount to ELOS guidelines) - Concept of for everything else may now become
important - New UAS technology can fall into the category of
everything else, as demonstrated by EM based
systems - RESULT
- Future paradigm shifts in approaches to aviation
will require high overhead response - RECOMMENDATION
- Encapsulate the general parameters of safe
aircraft operation and design in a way that
covers the everything else category
18Risk Analysis Artifacts (I) Preliminary Hazard
List
19Risk Analysis Artifacts (II)
Severity
- Catastrophic
- Critical
- Marginal
- Negligible
Likelihood
- Frequent
- Probable
- Occasional
- Remote
20UAS Propulsion SystemsGap Analysis / Risk
Analysis
21Wrapping Up
- Finalize Gap Analysis
- Determine recommendations
- Finalize documentation
- Touch up the spreadsheet
- Documentation on Risk Analysis
- Complete risk analysis
- Determine recommendations
- Draft up documentation, finalize
- Formalize everything into FAA doc format
22Review
- Project plan and schedule
- Project review up to last meet
- Summary of new efforts
- Description of plan to finish