Search Results

Matching Records: 5,084
1 2 3 4 5 6 7 8 9 10 Next >>
Sort Results By:
Selected   › View Selected  /  › Clear Selected
Technology Development Project Plan Phase 2 Unmanned Aircraft Systems (UAS) Integration in the National Airspace System (NAS) Integrated Aviation Systems Program (IASP)
Document ID: 20170003231
NTRS Full-Text: Click to View  [PDF Size: 2.6 MB]
Author: Sakahara, Robert D.; Grindle, Laurie
Abstract: The technology development Project Plan covers an overview of the Project and planned project hide
Publication Year: 2015
Document Type: Technical Report
Report/Patent Number: AFRC-E-DAA-TN37809
Date Acquired: Apr 20, 2017
X-43A: Adventures with a Hypersonic Airplane
Document ID: 20170003419
NTRS Full-Text: Click to View  [PDF Size: 6.1 MB]
Author: Purifoy, Dana; Neal, Bradford
Abstract: No abstract available
Publication Year: 2017
Document Type: Oral/Visual Presentation
Report/Patent Number: AFRC-E-DAA-TN40554
Date Acquired: Apr 17, 2017
Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design
Document ID: 20170003026
NTRS Full-Text: Click to View  [PDF Size: 1.3 MB]
Author: Ouellette, Jeffrey
Abstract: The communication of this method is being used by NASA in the ongoing collaborations with groups hide
Publication Year: 2017
Document Type: Oral/Visual Presentation
Report/Patent Number: AFRC-E-DAA-TN40222
Date Acquired: Apr 14, 2017
Dynamics and Control Work at NASA Armstrong
Document ID: 20170003027
NTRS Full-Text: Click to View  [PDF Size: 902 KB]
Author: Jacobson, Steve
Abstract: This presentation is a high level overview of Autonomy and Flexible Structures, like X-56 work being hide
Publication Year: 2017
Document Type: Oral/Visual Presentation
Report/Patent Number: AFRC-E-DAA-TN40542
Date Acquired: Apr 14, 2017
Modified Displacement Transfer Functions for Deformed Shape Predictions of Slender Curved Structures with Varying Curvatives
Document ID: 20140010280
NTRS Full-Text: Click to View  [PDF Size: 1.1 MB]
Author: Ko, William L.; Fleischer, Van Tran
Abstract: To eliminate the need to use finite-element modeling for structure shape predictions, a new method hide
Publication Year: 2014
Document Type: Technical Report
Report/Patent Number: NASA/TM-2014-216660, AFRC-E-DAA-TN13627
Date Acquired: Apr 04, 2017
Robust Modal Filtering and Control of the X-56A Model with Simulated Fiber Optic Sensor Failures
Document ID: 20170000223
NTRS Full-Text: Click to View  [PDF Size: 2.6 MB]
Author: Suh, Peter M.; Chin, Alexander W.; Mavris, Dimitri N.
Abstract: The X-56A aircraft is a remotely-piloted aircraft with flutter modes intentionally designed into the hide
Publication Year: 2016
Document Type: Technical Report
Report/Patent Number: NASA/TM-2016-219430, DFRC-E-DAA-TN36531
Date Acquired: Apr 04, 2017
Curved Displacement Transfer Functions for Geometric Nonlinear Large Deformation Structure Shape Predictions
Document ID: 20170001992
NTRS Full-Text: Click to View  [PDF Size: 3.4 MB]
Author: Ko, William L.; Fleischer, Van Tran; Lung, Shun-Fat
Abstract: For shape predictions of structures under large geometrically nonlinear deformations, Curved hide
Publication Year: 2017
Document Type: Technical Report
Report/Patent Number: NASA/TP-2017-219406, AFRC-E-DAA-TN26921
Date Acquired: Apr 04, 2017
Emerging Commercial UAS Operational Environments and NASA's Role
Document ID: 20170002615
NTRS Full-Text: Click to View  [PDF Size: 964 KB]
Author: Kim, Sam
Abstract: No abstract available
Publication Year: 2017
Document Type: Oral/Visual Presentation
Report/Patent Number: DFRC-E-DAA-TN40396
Date Acquired: Mar 31, 2017
Cohesive ARMD Full UAS Integration Strategy
Document ID: 20170002614
NTRS Full-Text: Click to View  [PDF Size: 4.1 MB]
Author: Hackenberg, Davis
Abstract: Introduction / Background; Current Landscape and Future Vision; UAS (Unmanned Aircraft System) hide
Publication Year: 2017
Document Type: Oral/Visual Presentation
Report/Patent Number: DFRC-E-DAA-TN39927
Date Acquired: Mar 31, 2017
Entry Descent and Landing Workshop Proceedings. Volume 1; Inflatable Reentry Vehicle Experiment-3 (IRVE-3) Project Overview & Instrumentation
Document ID: 20170002210
NTRS Full-Text: Click to View  [PDF Size: 1.0 MB]
Author: Dillman, Robert
Abstract: Entry mass at Mars is limited by the payload size that can be carried by a rigid capsule that can hide
Publication Year: 2015
Document Type: Oral/Visual Presentation
Report/Patent Number: DFRC-E-DAA-TN28396-4
Date Acquired: Mar 14, 2017
1 2 3 4 5 6 7 8 9 10 Next >>
Facebook icon, External Link to NASA STI page on Facebook Twitter icon, External Link to NASA STI on Twitter YouTube icon, External Link to NASA STI Channel on YouTube RSS icon, External Link to New NASA STI RSS Feed
Refine By
Search History
 
NASA Logo, External Link

NASA Official: Gerald Steeman

Sponsored By: NASA Scientific and Technical Information Program

Site Curator: STI Support Services

Last Modified: April 25, 2017

Privacy Policy & Important Notices Disclaimers, Copyright, Terms of Use Freedom of Information Act USA.gov NASA.gov NASA OCIO Free Adobe PDF Reader Free MS Word Viewer