The present invention models dynamic behavior of flight vehicles for
simulation, analysis, and design. The present invention allows a user to define the complexity of a
flight vehicle model, and such models may be simple
rigid body models, models of medium complexity, or very complex models including high order dynamics comprising hundreds of structural flexibility
modes and variables related to aero-elasticity, fuel sloshing, various types of effectors,
tail-wags-dog dynamics, complex
actuator models, load-torque feedback, wind gusts, and other parameters impacting flight vehicles. The present invention accommodates and analyzes multiple vehicle and
actuator concepts and configurations as defined in
flight vehicle input data, which specifies
flight vehicle parameters at a steady-state condition for modeling flight vehicle response to dynamic forces and flight control commands with respect to
steady state operation.