An integrated detection structure, comprising: - a first inertial mass and a second inertial mass, each of which has a main extension in a plane (xy) and is anchored to a substrate by means of respective elastic anchorage elements (8a-8b, 8a'-8b') in such a way as to be suspended above said substrate, said elastic anchorage elements (8a-8b, 8a'-8b') being configured to allow the respective inertial mass (2, 2') to perform a linear driving movement along a first axis (x) belonging to said plane (xy) and a respective first detection movement of rotation about a respective first axis of rotation (A, A') parallel to a second axis (y) belonging to said plane (xy), transverse to said first axis (x); - a first set of driving electrode (12, 12'), operatively coupled to each of said first and second inertial masses, configured to originate its respective driving movement, in opposite directions of said first axis (x) for said first and second inertial masses; and - a pair of first resonator elements (4a-4b, 4a'- 4b'; 3a-3b, 3a'-3b'), elastically connected to each of said first and second inertial masses, via respective elastic supporting elements (16; 8a-8b), said respective elastic supporting elements being configured to couple said first resonator elements to the respective one of said first and second inertial masses during the respective first movement of detection, and so as to enable an independent resonant movement thereof; wherein the respective first detection movement of said first inertial mass or second inertial mass is a function of the presence of a first angular velocity (Ω r; Ω z) or of a first linear acceleration (a z; a y) that is to be detected, and is designed to cause corresponding variations of resonance frequency of said first resonator elements (4a-4b, 4a'-4b'; 3a-3b, 3a'-3b'). - a first inertial mass and a second inertial mass, each of which has a main extension in a plane (xy) and is anchored to a substrate by means of respective elastic anchorage elements (8a-8b, 8a'-8b') in such a way as to be suspended above said substrate, said elastic anchorage elements (8a-8b, 8a'-8b') being configured to allow the respective inertial mass (2, 2') to perform a linear driving movement along a first axis (x) belonging to said plane (xy) and a respective first detection movement of rotation about a respective first axis of rotation (A, A') parallel to a second axis (y) belonging to said plane (xy), transverse to said first axis (x); - a first set of driving electrode (12, 12'), operatively coupled to each of said first and second inertial masses, configured to originate its respective driving movement, in opposite directions of said first axis (x) for said first and second inertial masses; and - a pair of first resonator elements (4a-4b, 4a'- 4b'; 3a-3b, 3a'-3b'), elastically connected to each of said first and second inertial masses, via respective elastic supporting elements (16; 8a-8b), said respective elastic supporting elements being configured to couple said first resonator elements to the respective one of said first and second inertial masses during the respective first movement of detection, and so as to enable an independent resonant movement thereof; wherein the respective first detection movement of said first inertial mass or second inertial mass is a function of the presence of a first angular velocity (Ω r; Ω z) or of a first linear acceleration (a z; a y) that is to be detected, and is designed to cause corresponding variations of resonance frequency of said first resonator elements (4a-4b, 4a'-4b'; 3a-3b, 3a'-3b').