Launch Vehicle Ascent Trajectory Simulation Using the Program to Optimize Simulated Trajectories II (POST2)The Program to Optimize Simulated Trajectories II (POST2) has been continuously developed for over 40 years and has been used in many flight and research projects. Recently, there has been an effort to improve the POST2 architecture by promoting modularity, flexibility, and ability to support multiple simultaneous projects. The purpose of this paper is to provide insight into the development of trajectory simulation in POST2 by describing methods and examples of various improved models for a launch vehicle liftoff and ascent.
Document ID
20170001620
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Lugo, Rafael A. (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Shidner, Jeremy D. (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Powell, Richard W. (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Marsh, Steven M. (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Hoffman, James A. (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Litton, Daniel K. (NASA Langley Research Center Hampton, VA, United States)
Schmitt, Terri L. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
February 16, 2017
Publication Date
February 5, 2017
Subject Category
Astrodynamics
Report/Patent Number
NF1676L-25552Report Number: NF1676L-25552
Meeting Information
Meeting: AAS/AIAA Space Flight Mechanics Meeting
Location: San Antonio, TX
Country: United States
Start Date: February 5, 2017
End Date: February 9, 2017
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics