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Proceedings of the 3rd Annual International Conference on Mechanics and Mechanical Engineering (MME 2016)
The linear parameter varying (LPV) system model of the lateral-directional dynamics for large envelope flight of modular aircraft including various configurations was built. The validity of the aircraft LPV model was verified by the comparison of dynamic simulation between the LPV model and the nonlinear model. The lateral-directional dynamic characteristics under different configurations of modular aircraft in large flight envelope were studied. The stability augmentation system (SAS) for thedoi:10.2991/mme-16.2017.1 fatcat:mfhyz5hrrbcotmxq4vgkhqyg5e