damaged aircraft. Three damage-configurations are studied at supersonic speeds. The methodology can be used to quickly generate aerodynamic model for damaged aircraft for simulation and reconfigurable control. See also Missile Datcom USAF Stability and Control DATCOM References Williams, John E., Vukelich, Steven R. "The USAF Stability and Control Digital DATCOM. Volume I. Users Manual." AFFDL-TR-79-3032 Volume I, Nov. 1979. Williams, John E., Vukelich, Steven R. "The USAF Stability and Control Digital DATCOM. Volume II. Implementation of Datcom Methods." AFFDL-TR-79-3032 Volume II, Nov. 1979. Williams, John E., Vukelich, Steven R. "The USAF Stability and Control Digital DATCOM. Volume III. Plot Module." AFFDL-TR-79-3032 Volume III, Nov. 1979. Blake, W. B. "Prediction of Fighter Aircraft Dynamic Derivatives Using Digital Datcom," AIAA 3rd Applied Aerodynamics Conference, AIAA-1985-4070, Colorado Spring, CO, October 1985. The Mathworks, Inc. "Model-Based Design of a New Light-weight Aircraft," AIAA Modeling and Simulation Technologies Conference and Exhibit, AIAA-2007-6371, Hilton Head, SC, August 2007. Siddiqui, B.A. and Kassem, A. H., "Using USAF DATCOM to Predict Nonlinear Aerodynamics of Structurally Impaired Aircraft", International Review of Aerospace Engineering (I.RE.AS.E), January 2010. External links OpenDatcom Digital DATCOM at Embry-Riddle Aeronautical University Yahoo Digital_Datcom Group Air Force Research Laboratory Control Theory Optimization Branch Aerospace Toolbox for MATLAB JSBSim FlightGear 1965-Datcom-Sections-1-5 1965-Datcom-Sections-6-9 AFRL-TR-79-3032 USAF DATCOM User's Manual, Volume 1 AFRL-TR-79-3032 USAF DATCOM User's Manual, Volume 2 AFRL-TR-79-3032 USAF DATCOM User's Manual, Volume 3 AFWAL-TR083-3048 McDonnell Douglas Corporation Final Report for DATCOM, April 1978 Aerospace engineering software Aerodynamics Aircraft controls Fortran software Wright-Patterson Air Force Base