Publication Date:
2019-08-13
Description:
The Ares I-X trajectory reconstruction produced best estimated trajectories of the flight test vehicle ascent through stage separation, and of the first and upper stage entries after separation. The trajectory reconstruction process combines on-board, ground-based, and atmospheric measurements to produce the trajectory estimates. The Ares I-X vehicle had a number of on-board and ground based sensors that were available, including inertial measurement units, radar, air-data, and weather balloons. However, due to problems with calibrations and/or data, not all of the sensor data were used. The trajectory estimate was generated using an Iterative Extended Kalman Filter algorithm, which is an industry standard processing algorithm for filtering and estimation applications. This paper describes the methodology and results of the trajectory reconstruction process, including flight data preprocessing and input uncertainties, trajectory estimation algorithms, output transformations, and comparisons with preflight predictions.
Keywords:
Launch Vehicles and Launch Operations
Type:
NF1676L-11837
,
58th JANNAF Propulsion Meeting; Apr 18, 2011 - Apr 22, 2011; Arlington, VA; United States|32nd Exhaust Plume and Signatures Meeting; Apr 18, 2011 - Apr 22, 2011; Arlington, VA; United States|32nd Airbreathing Propulsion Meeting; Apr 18, 2011 - Apr 22, 2011; Arlington, VA; United States|44th Combustion Meeting; Apr 18, 2011 - Apr 22, 2011; Arlington, VA; United States
Format:
application/pdf
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