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Model Fidelity Studies for Rapid Trajectory Optimization.

Conference ·
DOI:https://doi.org/10.2514/6.2019-0430· OSTI ID:1582127
; ;
Abstract not provided.
Research Organization:
Sandia National Laboratories (SNL-NM), Albuquerque, NM (United States)
Sponsoring Organization:
USDOE National Nuclear Security Administration (NNSA)
DOE Contract Number:
AC04-94AL85000
OSTI ID:
1582127
Report Number(s):
SAND2019-0031C; 671232
Country of Publication:
United States
Language:
English

References (21)

Integrals of the motion for optimal trajectories in atmospheric flight conference February 2013
Rapid Simultaneous Hypersonic Aerodynamic and Trajectory Optimization Using Variational Methods conference June 2012
Aerodynamic Surrogate Modeling of Variable Geometry
  • Crowley, Daniel; Robertson, Bradford; Douglas, Rebecca
  • 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition https://doi.org/10.2514/6.2012-268
conference November 2012
Dakota, a multilevel parallel object-oriented framework for design optimization, parameter estimation, uncertainty quantification, and sensitivity analysis version 6.0 theory manual report May 2014
Rapid Three-Dimensional Constrained Trajectory Generation for Near Space Hypersonic Vehicles conference September 2012
Direct trajectory optimization by a Chebyshev pseudospectral method
  • Fahroo, F.; Ross, I. M.
  • Proceedings of 2000 American Control Conference (ACC 2000), Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334) https://doi.org/10.1109/ACC.2000.876945
conference January 2000
Guess-Free Trajectory Optimization conference June 2012
Extension of a Pseudospectral Legendre Method to Non-Sequential Multiple-Phase Optimal Control Problems conference June 2012
Advances in Highly Constrained Multi-Phase Trajectory Generation using the General Pseudospectral Optimization Software (GPOPS) conference August 2013
Adaptive Sampling to Improve Aerodynamic Predictions for Reusable Rocket-Powered Vehicles conference September 2013
A Method for Launch Vehicle Performance Analysis via Surrogate Modeling conference January 2016
Constrained Trajectory Optimization Using Pseudospectral Methods conference June 2012
Verification of a CFD Procedure for Aerodynamic Database Development Using the Hyper-X Stack Configuration conference June 2012
Aerodynamic database development for the Hyper-X airframe integrated scramjet propulsion experiments conference February 2013
Towards Real-Time Computation of Optimal Controls for Nonlinear Systems conference June 2012
A Comparison between Trajectory Optimization Methods: Differential Dynamic Programming and Pseudospectral Optimal Control conference January 2016
X-43 - Scramjet Power Breaks the Hypersonic Barrier: Dryden Lectureship in Research for 2006 conference June 2012
Rapid Trajectory Optimization Using Computational Intelligence for Guidance and Conceptual Design of Multistage Space Launch Vehicles conference June 2012
Hyper-X Post-Flight Trajectory Reconstruction conference June 2012
INVENT Surrogate Modeling and Optimization of Transient Thermal Responses
  • Miller, Cameron; Maser, Adam; Garcia, Elena
  • 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition https://doi.org/10.2514/6.2012-1123
conference November 2012
On-Line Trajectory Optimization for Autonomous Air Vehicles conference June 2012

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