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Stratospheric airships have introduced interesting solutions for challenges in aerospace industries. Buoyant and propulsion forces produced by airships makes them to be capable of long-time flight and efficient operation. In spite of many progresses, there are still many challenges in this interesting field of study. In this paper, first the dynamic model of fully-actuated stratospheric airship with 6-DOF expressed by the generalized coordinates, then desired values of the airship attitude, linear and angular velocities obtained according to desired path and using pseudo inversion of the kinematics and dynamics equations. In view of the unknown inertial parameters first in adaptive inverse dynamic control, inertial parameters estimated online by using linearization parameters and gradient update law. Next control law and nonlinear dynamic equation is deduced by designing control algorithm based on passivity, and according to that, adaptive and robust control based on passivity applied for controlling airship. The stability of the closed loop control system is proved by using the Lyapunov stability theory. Finally, comparison between the results of the all methods are shown.