NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Improvement of Automated POST Case Success Rate Using Support Vector MachinesDuring early conceptual design of complex systems, concept down selection can have a large impact upon program life-cycle cost. Therefore, any concepts selected during early design will inherently commit program costs and affect the overall probability of program success. For this reason it is important to consider as large a design space as possible in order to better inform the down selection process. For conceptual design of launch vehicles, trajectory analysis and optimization often presents the largest obstacle to evaluating large trade spaces. This is due to the sensitivity of the trajectory discipline to changes in all other aspects of the vehicle design. Small deltas in the performance of other subsystems can result in relatively large fluctuations in the ascent trajectory because the solution space is non-linear and multi-modal. In order to help capture large design spaces for new launch vehicles, the authors have performed previous work seeking to automate the execution of the industry standard tool, Program to Optimize Simulated Trajectories (POST). This work initially focused on implementation of analyst heuristics to enable closure of cases in an automated fashion, with the goal of applying the concepts of design of experiments (DOE) and surrogate modeling to enable near instantaneous throughput of vehicle cases.3 As noted in [4] work was then completed to improve the DOE process by utilizing a graph theory based approach to connect similar design points.
Document ID
20170012302
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Zwack, Mathew R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Dees, Patrick D.
(Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Date Acquired
December 18, 2017
Publication Date
September 12, 2017
Subject Category
Launch Vehicles And Launch Operations
Astrodynamics
Report/Patent Number
M17-6198
Meeting Information
Meeting: AIAA Space 2017 Conference & Exposition
Location: Orlando, FL
Country: United States
Start Date: September 12, 2017
End Date: September 14, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNM12AA41C
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available