A three axis gyroscope, comprising: - a first gyroscope structure, and - a second gyroscope structure, wherein one of the first and second gyroscope structures comprises a two axis gyroscope structure and another of the first and second gyroscope structures comprises a one axis gyroscope structure, wherein - said two axis gyroscope structure is configured to be driven into a first linear drive mode oscillation in the x-axis direction within a plane of the essentially planar three axis gyroscope by exciting with driving actuators and a first pair of proof masses of the two axis gyroscope structure is configured to be driven into a linear detection motion in the y-axis direction by angular velocity about the z-axis, - said one axis gyroscope structure is configured to be driven by coupling into a second linear drive mode oscillation in the y-axis direction within the plane of the three axis gyroscope; and - a lever spring system coupling a first linear drive mode oscillation of said first gyroscope structure and a second linear drive mode oscillation of said second gyroscope structure into one combined primary motion, characterized in that the three axis gyroscope further comprises: - a second pair of proof masses of the two axis gyroscope structure configured to be driven into a linear detection motion in the z-axis direction by angular velocity about the y-axis, wherein - a pair of proof masses of the one axis gyroscope structure is configured to be driven into a linear detection motion in the z-axis direction by angular velocity about the x-axis, and wherein at least one pair of proof masses is mutually coupled with a lever allowing linear detection motion of the mutually coupled pair of proof masses in opposite phase and preventing linear detection motion of the mutually coupled pair of proof masses in the same phase. - a first gyroscope structure, and - a second gyroscope structure, - said two axis gyroscope structure is configured to be driven into a first linear drive mode oscillation in the x-axis direction within a plane of the essentially planar three axis gyroscope by exciting with driving actuators and a first pair of proof masses of the two axis gyroscope structure is configured to be driven into a linear detection motion in the y-axis direction by angular velocity about the z-axis, - said one axis gyroscope structure is configured to be driven by coupling into a second linear drive mode oscillation in the y-axis direction within the plane of the three axis gyroscope; and - a lever spring system coupling a first linear drive mode oscillation of said first gyroscope structure and a second linear drive mode oscillation of said second gyroscope structure into one combined primary motion, - a second pair of proof masses of the two axis gyroscope structure configured to be driven into a linear detection motion in the z-axis direction by angular velocity about the y-axis, wherein - a pair of proof masses of the one axis gyroscope structure is configured to be driven into a linear detection motion in the z-axis direction by angular velocity about the x-axis, and wherein at least one pair of proof masses is mutually coupled with a lever allowing linear detection motion of the mutually coupled pair of proof masses in opposite phase and preventing linear detection motion of the mutually coupled pair of proof masses in the same phase.