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Real-Time Simulation and Control of Flexible Launch Vehicles

The target of this project is to develop real-time simulation and control tools for flexile launch vehicles. Both the direct numerical integration scheme and indirect dynamic beam solution (based-on sensor measurement data) are sought. Moreover, they are both constrained by the requirement of delivering "real-time" solutions for further control studies.

Optimum Wing Shape

Sponsor: NASA Kennedy Space Center (KSC) and a.i. solutions, Inc.

Publications: (Refer to the publication page for detailed paper links)

  1. Su, W., King, C. K., Clark, S. R., Griffin, E. D., Suhey, J. D., and Wolf, M. G., “Dynamic Beam Solutions for Real-Time Simulation and Control Development of Flexible Rockets,” AIAA-2016-1954, Proceedings of the 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (at AIAA SciTech 2016), San Diego, CA, Jan. 4–8, 2016.
  2. Su, W., King, C. K., Clark, S. R., Griffin, E. D., Suhey, J. D., and Wolf, M. G., “Dynamic Beam Solutions for Real-Time Simulation and Control Development of Flexible Rockets,” Journal of Spacecraft and Rockets, in press.
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Last updated: 01/23/2016
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