Recent experiences of the NASA Engineering and Safety Center (NESC) Guidance Navigation and Control (GN&C) Technical Discipline Team (TDT) PDF Download
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Author: Cornelius J. Dennehy
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
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Author: Cornelius J. Dennehy
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
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Book Description
Author: National Aeronaut Administration (Nasa)
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
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Book Description
Technical Report Dennehy, Cornelius J. Langley Research Center NASA/TM-2011-217083, L-20018, NF1676L-12566 WBS 869021.03.07.01.03 GUIDANCE (MOTION); HUMAN RESOURCES; KNOWLEDGE BASED SYSTEMS; RISK; NAVIGATION; SAFETY; INDUSTRIES; UNIVERSITIES; ORGANIZATIONS
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781794068049
Category : Science
Languages : en
Pages : 44
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Book Description
The NASA Engineering and Safety Center (NESC) is an independently funded NASA Program whose dedicated team of technical experts provides objective engineering and safety assessments of critical, high risk projects. NESC's strength is rooted in the diverse perspectives and broad knowledge base that add value to its products, affording customers a responsive, alternate path for assessing and preventing technical problems while protecting vital human and national resources. The Guidance Navigation and Control (GN&C) Technical Discipline Team (TDT) is one of fifteen such discipline-focused teams within the NESC organization. The TDT membership is composed of GN&C specialists from across NASA and its partner organizations in other government agencies, industry, national laboratories, and universities. This paper will briefly define the vision, mission, and purpose of the NESC organization. The role of the GN&C TDT will then be described in detail along with an overview of how this team operates and engages in its objective engineering and safety assessments of critical NASA. NASA/TM-2011-217083, L-20018, NF1676L-12566 Dennehy, Cornelius J. Langley Research Center
Author: Nasa Technical Reports Server (Ntrs)
Publisher: BiblioGov
ISBN: 9781289127602
Category :
Languages : en
Pages : 46
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Book Description
The NASA Engineering and Safety Center (NESC) is an independently funded NASA Program whose dedicated team of technical experts provides objective engineering and safety assessments of critical, high risk projects. NESC's strength is rooted in the diverse perspectives and broad knowledge base that add value to its products, affording customers a responsive, alternate path for assessing and preventing technical problems while protecting vital human and national resources. The Guidance Navigation and Control (GN&C) Technical Discipline Team (TDT) is one of fifteen such discipline-focused teams within the NESC organization. The TDT membership is composed of GN&C specialists from across NASA and its partner organizations in other government agencies, industry, national laboratories, and universities. This paper will briefly define the vision, mission, and purpose of the NESC organization. The role of the GN&C TDT will then be described in detail along with an overview of how this team operates and engages in its objective engineering and safety assessments of critical NASA.
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781793903020
Category : Science
Languages : en
Pages : 30
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Book Description
This paper will briefly define the vision, mission, and purpose of the NESC organization. The role of the GN&C TDT will then be described in detail along with an overview of how this team operates and engages in its objective engineering and safety assessments of critical NASA projects. This paper will then describe key issues and findings from several of the recent GN&C-related independent assessments and consultations performed and/or supported by the NESC GN&C TDT. Among the examples of the GN&C TDT s work that will be addressed in this paper are the following: the Space Shuttle Orbiter Repair Maneuver (ORM) assessment, the ISS CMG failure root cause assessment, the Demonstration of Autonomous Rendezvous Technologies (DART) spacecraft mishap consultation, the Phoenix Mars lander thruster-based controllability consultation, the NASA in-house Crew Exploration Vehicle (CEV) Smart Buyer assessment and the assessment of key engineering considerations for the Design, Development, Test & Evaluation (DDT&E) of robust and reliable GN&C systems for human-rated spacecraft. Dennehy, Cornelius J. Goddard Space Flight Center; Langley Research Center WBS 510505.06.07.03.99
Author: Cornelius J. Dennehy
Publisher: BiblioGov
ISBN: 9781289236519
Category :
Languages : en
Pages : 32
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Book Description
This paper will briefly define the vision, mission, and purpose of the NESC organization. The role of the GN&C TDT will then be described in detail along with an overview of how this team operates and engages in its objective engineering and safety assessments of critical NASA projects. This paper will then describe key issues and findings from several of the recent GN&C-related independent assessments and consultations performed and/or supported by the NESC GN&C TDT. Among the examples of the GN&C TDT s work that will be addressed in this paper are the following: the Space Shuttle Orbiter Repair Maneuver (ORM) assessment, the ISS CMG failure root cause assessment, the Demonstration of Autonomous Rendezvous Technologies (DART) spacecraft mishap consultation, the Phoenix Mars lander thruster-based controllability consultation, the NASA in-house Crew Exploration Vehicle (CEV) Smart Buyer assessment and the assessment of key engineering considerations for the Design, Development, Test & Evaluation (DDT&E) of robust and reliable GN&C systems for human-rated spacecraft.
Author: Kang-Lin Peng
Publisher: Springer Nature
ISBN: 9819716063
Category :
Languages : en
Pages : 186
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Author: Nasa Technical Reports Server (Ntrs)
Publisher: BiblioGov
ISBN: 9781289066635
Category :
Languages : en
Pages : 40
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Book Description
The Guidance, Navigation, and Control (GN&C) Technical Discipline Team (TDT) sponsored Dr. J. Russell Carpenter, a Navigation and Rendezvous Subject Matter Expert (SME) from NASA's Goddard Space Flight Center (GSFC), to provide support to the Defense Advanced Research Project Agency (DARPA) Orbital Express (OE) rendezvous and docking flight test that was conducted in 2007. When that DARPA OE mission was completed, Mr. Neil Dennehy, NASA Technical Fellow for GN&C, requested Dr. Carpenter document his findings (lessons learned) and recommendations for future rendezvous missions resulting from his OE support experience. This report captures lessons specifically from anomalies that occurred during one of OE's unmated operations.
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781793960306
Category : Science
Languages : en
Pages : 38
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Book Description
The Guidance, Navigation, and Control (GN&C) Technical Discipline Team (TDT) sponsored Dr. J. Russell Carpenter, a Navigation and Rendezvous Subject Matter Expert (SME) from NASA's Goddard Space Flight Center (GSFC), to provide support to the Defense Advanced Research Project Agency (DARPA) Orbital Express (OE) rendezvous and docking flight test that was conducted in 2007. When that DARPA OE mission was completed, Mr. Neil Dennehy, NASA Technical Fellow for GN&C, requested Dr. Carpenter document his findings (lessons learned) and recommendations for future rendezvous missions resulting from his OE support experience. This report captures lessons specifically from anomalies that occurred during one of OE's unmated operations. Dennehy, Cornelius J. and Carpenter, James R. Goddard Space Flight Center; Langley Research Center NASA/TM-2011-217088, NESC-RP-10-00628, L-20025, NF1676L-12667
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781719383752
Category :
Languages : en
Pages : 32
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Book Description
The National Aeronautics and Space Administration Engineering and Safety Center designed, developed and flew the alternative Max Launch Abort System (MLAS) as risk mitigation for the baseline Orion spacecraft launch abort system already in development. The NESC was tasked with both formulating a conceptual objective system design of this alternative MLAS as well as demonstrating this concept with a simulated pad abort flight test. Less than 2 years after Project start the MLAS simulated pad abort flight test was successfully conducted from Wallops Island on July 8, 2009. The entire flight test duration was 88 seconds during which time multiple staging events were performed and nine separate critically timed parachute deployments occurred as scheduled. This paper provides an overview of the guidance navigation and control technical approaches employed on this rapid prototyping activity; describes the methodology used to design the MLAS flight test vehicle; and lessons that were learned during this rapid prototyping project are also summarized. Dennehy, Cornelius J. and Lanzi, Raymond J. and Ward, Philip R. Goddard Space Flight Center; Langley Research Center; Wallops Flight Facility FLIGHT TEST VEHICLES; NAVIGATION; GUIDANCE (MOTION); AERONAUTICAL ENGINEERING; FLIGHT TESTS; SPACECRAFT LAUNCHING; SAFETY; NASA PROGRAMS; PARACHUTES; SYSTEMS ENGINEERING; RISK
