No abstract

This paper describes a generic, state-of-the-art, high. performanceaircraft model, including detailed, fullenvelope, nonlinear aer_ynamics, and full-envelope thrust andfirst-order engine response data. While this model was primarily developed for the AIAA Controls Design Challenge, the availability of such a model provides a common focusforrc_ch inac_nautical control theory and methodology. This paper also describes an implementation of this model using the FORTRAN computer language, associated routines furnished withtheaircraft model, andtechniques for interfacing these routines toexternal procedures. R rudder r yaw rate s stability axis z along the z-body axis Y sideforce It along the p-body axis z along the z-body axis 0 standard day, sea level conditions 14. SUBJECT TERMS Simulation; Controls; Design challenge; Model; Numerical simulation 17. SECURITY CLASSIFICATION 111. SECURITY CLASSIFICATION

No abstract