Keywords: Aerospace; launcher staging separation
Proceedings of the 10th International Modelica Conference; March 10-12; 2014; Lund; Sweden
 Decker, J. P. Experimental Aerodynamics and Analysis of the Stage Separation of Reusable Launch Vehicles. NASASP-148, January 1967.
 Decker, J. P., and Gera, J. An Exploratory Study of Parallel-Stage Separation of Reusable Launch Vehicles. NASA TN D-4765, October 1968.
 Baumgarte, J. Stabilization of Constraints and Integrals of Motion in Dynamical Systems. Computer Methods in Applied Mechanics and Engineering, Vol. 1, No. 1, 1972, pp. 1-16.
 Decker, J.P., and Wilhite, A. W. Technology and Methodology of Separating Two Similar Size Aerospace Vehicles Within the Atmosphere.AIAA Paper 1975-29, Jan. 1975.
 Bauer, G.L., Cornick, D.E., and Stevenson, R. Capabilities and Applications of the Program to Optimize Simulated Trajectories (POST). NASA CR-2770, 1977.
 Ascher, U.M., Chin, H., Petzold, L.R., and Reich, S. Stabilization of constrained mechanical systems with DAEs and invariant manifolds. Journal ofMechanics of tructures and Machines, Vol. 23, 1994, pp 135-157.
 Elmqvist, H., Mattson, S.E., and Otter, M. Modelica - An International Effort to Design an Object-Oriented Modeling Language. Summer Computer Simulation Conference, pp. 333-339, 1998, ISBN 1-56555-149-4.
 Mattson, S.E., Elmqvist, H., and Otter, M. Physical system modeling with Modelica. Control Engineering Practice, v. 6, pp. 501-510, 1998.
 Otter, M., Elmqvist, H., and Mattsson, S.E. The New Modelica Multibody Library. Proceedings of the 3rd International Modelica Conference, Link√∂ping, 2003, p 311-330.
 Tartabini, P. V., Bose, D. M., McMinn, J. D., Martin, J. G., and Strovers, B. K. Hyper-X Stage Separation Trajectory Validation Studies. AIAA Paper 2003-5819, August 2003.
 Murphy, K.J., Buning, P.G., Pamadi, B.N., Scallion, W.I., and Jones, K.M. Status of Stage Separation Tool Development for Next Generation Launch Vehicle Technologies. AIAA Paper 2004-2595.
 Pamadi, B.N., Neirynck, T. A., Covell, P.F., Hotchko, N.J., and Bose, D.M. Simulation and Analyses of StagingManeuvers of Next Generation Reusable Launch Vehicles. AIAA Paper 2004-5185.
 Pamadi, B.N., Hotchko, N.J., Jamshid Samareh, Covell, P.F., and Tartabini, P.V. Simulation and Analyses of Multi- Body Separation in Launch Vehicle Staging Environment. AIAA Paper 2006-8033.
 Pamadi, B.N., Neirynck, T. A., Hotchko, N.J., Scallion W.I., Murphy, K.J., and Covell, P.F. Simulation and Analyses of Stage Separation of Two-Stage Reusable Launch Vehicles. Journal of Spacecraft and Rockets, Vol. 44, No. 1, January-February 2007, pp 66-80.
 K√§lldahl M. Separation Analysis with OpenModelica. Student thesis, Link√∂ping University, Department of Electrical Engineering, Institutionen f¬®r systemteknik, Sweden, 2007.
 Toniolo, M., Tartabini, P.V., and Pamadi, B.N. Constraint Force Equation Methodology for Modeling Multi-Body Stage Separation Dynamics. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008, 10.2514/6.2008-219.
 Tartabini, P.V., Roithmayr, C.M., Toniolo,M.D., Karlgaard, C.D., and Pamadi, B. N. Modeling Multibody Stage Separation Dynamics Using Constraint Force Equation Methodology. Journal of Spacecraft and Rockets, Vol. 48, No. 4, July-August 2011, pp 573-583.
 Pamadi, B.N., Tartabini, P.V., Toniolo, M.D., Roithmayr, C.M., Karlgaard, C.D., and Samareh, J.A. Application of Constraint Force EquationMethodology for Launch Vehicle Stage Separation. Journal of Spacecraft and Rockets, Vol. 50, No. 1, January-February 2013, pp 191-205.