Jeb S Orr
Jeb S Orr
Flight Systems Principal Staff at Mclaurin Aerospace
Verified email at nasa.gov
Title
Cited by
Cited by
Year
Robust, practical adaptive control for launch vehicles
J Orr, T Van Zwieten
AIAA Guidance, Navigation, and Control Conference, 4549, 2012
232012
High-efficiency thrust vector control allocation
JS Orr, NJ Slegers
Journal of Guidance, Control, and Dynamics 37 (2), 374-382, 2014
182014
State space implementation of linear perturbation dynamics equations for flexible launch vehicles
J Orr, M Johnson, J Wetherbee, J McDuffie
AIAA Guidance, Navigation, and Control Conference, 5962, 2009
182009
Space launch system ascent flight control design
JS Orr, JH Wall, TS VanZwieten, CE Hall
172014
Space launch system implementation of adaptive augmenting control
JH Wall, JS Orr, TS VanZwieten
152014
Flexible modes control using sliding mode observers: Application to Ares I
Y Shtessel, C Hall, S Baev, J Orr
AIAA guidance, navigation, and control conference, 7565, 2010
152010
Lunar spacecraft powered descent control using higher-order sliding mode techniques
JS Orr, YB Shtessel
Journal of the Franklin Institute 349 (2), 476-492, 2012
142012
Adaptive Augmenting Control Flight Characterization Experiment on an F/A-18
TS VanZwieten, ET Gilligan, JH Wall, JS Orr, CJ Miller, CE Hanson
102014
A coupled aeroelastic model for launch vehicle stability analysis
J Orr
AIAA atmospheric flight mechanics conference, 7642, 2010
92010
Optimal recursive digital filters for active bending stabilization
JS Orr
82013
A Flight Dynamics Model for a Multi-Actuated Flexible Rocket Vehicle
J Orr
AIAA Atmospheric Flight Mechanics Conference, 6563, 2011
72011
Robust Control of Lunar Spacecraft Powered Descent Using a Second Order Sliding Mode Technique
J Orr, Y Shtessel
AIAA Guidance, Navigation and Control Conference and Exhibit, 6815, 2008
52008
Space Launch System Flight Control
JS Orr
42012
Elastic Model Transitions Using Quadratic Inequality Constrained Least Squares
J Orr
AIAA Modeling and Simulation Technologies Conference, 4561, 2012
42012
Analysis of the X-15 Flight 3-65-97 Divergent Limit-Cycle Oscillation
JS Orr, CJ Dennehy
Journal of Aircraft 54 (1), 135-148, 2017
32017
A comprehensive analysis of the X-15 Flight 3-65 accident
CJ Dennehy, JS Orr, I Barshi, IC Statler
32014
Robust Lunar Spacecraft Autopilot Design Using High Order Sliding Mode Control
J Orr, Y Shtessel
AIAA Guidance, Navigation, and Control Conference, 6182, 2009
32009
In-Flight Suppression of a Destabilized F/A-18 Structural Mode Using the Space Launch System Adaptive Augmenting Control System
JH Wall, CJ Miller, CE Hanson, TS Van Zwieten, J Orr, E Gilligan
AIAA Guidance, Navigation, and Control Conference, 1775, 2015
22015
Lattice Boltzmann Method for Spacecraft Propellant Slosh Simulation
JS Orr, JF Powers, HQ Yang
12015
The Human Factors of an early space accident: Flight 3-65 of the X-15.
I Barshi, IC Statler, JS Orr
Space Safety is No Accident, 267-275, 2015
12015
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