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A Flight-Mechanics Solver For Aircraft Inverse Simulations And Application To 3D Mirage-Iii Maneuver
The main objective of this paper is to present a general mathematical model and an associated numerical algorithm applicable to an arbitrary fixed-wing fixed-mass aircraft undergoing an arbitrary maneuver, based on the 3D nonlinear coupled differential-algebraic equations of motion, including force, moment, kinematic and constraint equations. The model is formulated to address the inverse simulation problem where a target maneuver is prescribed and the corresponding time dependent patterns ofdoi:10.5281/zenodo.1346086 fatcat:5cnqr7mpxnbgtfbg2rjkgvnkva