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Methods for Determining the Level of Autonomy to Design into a Human Spaceflight Vehicle: A Function Specific ApproachThe next-generation human spaceflight vehicle is in a unique position to realize the benefits of more than thirty years of technological advancements since the Space Shuttle was designed. Computer enhancements, the emergence of highly reliable decision-making algorithms, and an emphasis on efficiency make an increased use of autonomous systems highly likely. NASA is in a position to take advantage of these advances and apply them to the human spaceflight environment. One of the key paradigm shifts will be the shift, where appropriate, of monitoring, option development, decision-making, and execution responsibility from humans to an Autonomous Flight Management (AFM) system. As an effort to reduce risk for development of an AFM system, NASA engineers are developing a prototype to prove the utility of previously untested autonomy concepts. This prototype, called SMART (Spacecraft Mission Assessment and Replanning Tool), is a functionally decomposed flight management system with an appropriate level of autonomy for each of its functions. As the development of SMART began, the most important and most often asked question was, How autonomous should an AFM system be? A thorough study of the literature through 2002 surrounding autonomous systems has not yielded a standard method for designing a level of autonomy into either a crewed vehicle or an uncrewed vehicle. The current focus in the literature on defining autonomy is centered on developing IQ tests for built systems. The literature that was analyzed assumes that the goal of all systems is to strive for complete autonomy from human intervention, rather than identifying how autonomous each function within the system should have been. In contrast, the SMART team developed a method for determining the appropriate level of autonomy to be designed into each function within a system. This paper summarizes the development of the Level of Autonomy Assessment Tool and its application to the SMART project.
Document ID
20100017272
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Proud, Ryan W.
(NASA Johnson Space Center Houston, TX United States)
Hart, Jeremy J.
(NASA Johnson Space Center Houston, TX United States)
Mrozinski, Richard B.
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
August 24, 2013
Publication Date
September 1, 2003
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
JSC-CN-8129
AD-A515467
Meeting Information
Meeting: Performance Metrics for Intelligent Systems
Location: Gaithersburg, MD
Country: United States
Start Date: September 16, 2003
End Date: September 18, 2003
Sponsors: National Inst. of Standards and Technology
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
AFM (AUTONOMOUS FLIGHT MANAGEMENT)
AUTONOMOUS SYSTEMS
INTELLIGENT SYSTEMS
OODA (OBSERVE ORIENT DECIDE AND ACT)
AUTONOMY
MISSION OPERATIONS
TRAJECTORY MANAGEMENT
DESIGN PHASE
FLIGHT OPERATIONS
HUMAN COMPUTER INTERACTION
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