Device and method for measuring non-isoplanatism wave-front errors and turbulence characteristic parameters of atmosphere turbulence
A technique for atmospheric turbulence and wavefront error, applied in the field of optical information measurement, can solve the problems of high engineering requirements and inability to obtain two-dimensional distribution information of turbulent non-isohalo wavefront error
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Embodiment 1
[0044] The atmospheric turbulent non-isohalotic wavefront error and turbulent characteristic parameter measuring device of the present invention mainly includes a telescope 1, a light splitting module 2, a beam shrinking module 3, a target Hartmann sensor 4 and a corresponding wavefront processor 6, Beacon Hartmann sensor 5 and its corresponding wavefront processor 7 . Wherein, the spectroscopic module 2 is composed of a spectroscopic mirror 21 and a reflecting mirror 22, which can exchange positions with each other. The attenuator module 3 can be used as figure 2 The transmissive structure shown in (a) can also be used as figure 2 (b) and (c) respectively show the reflection structure, reflection and transmission combined structure. The beam splitting module 2 and the beam shrinking module 3 can also exchange positions with each other, that is, the method of first splitting the beam and then shrinking the beam, or the method of first reducing the beam and then splitting t...
Embodiment 2
[0087] Such as Figure 6 Shown is a specific implementation of the measurement device and method of the atmospheric turbulence anisotropic wavefront error and turbulence characteristic parameters of the present invention to realize the angular anisotropic wavefront error measurement in the natural beacon mode.
[0088]The device consists of a telescope 1, a spectroscopic module 2, a beam reduction module 3, a target Hartmann sensor 4 and its corresponding wavefront processor 6, a beacon Hartmann sensor 5 and its corresponding wavefront processor 7, etc. composition. In this embodiment, the beam splitting module 2 is composed of a beam splitter 21 and a reflector 22 ; the beam shrinking module 3 is composed of two identical transmission beam shrinking mirror groups 31 and 32 . The target Hartmann sensor 4 is mainly composed of a microlens group 43, a matching lens 44 and a CCD camera 45, and a filter 41 is placed in the center of the optical path perpendicular to its optical a...
Embodiment 3
[0098] Such as Figure 7 Shown is a specific implementation of the measurement device and method of atmospheric turbulence anisotropic wavefront error and turbulence characteristic parameters of the present invention to realize the measurement of angle and focus comprehensive anisotropic wavefront error in artificial beacon mode.
[0099] The external structure of the artificial beacon angle and focus integrated anisotropic wavefront error device provided in this embodiment is the same as that in Embodiment 2. Due to the characteristic wavelength of the artificial beacon, the difference between this embodiment and embodiment 2 is that the filter 41 in the target Hartmann sensor 4 and the filter 51 in the beacon Hartmann sensor 5 in embodiment 1 are respectively Replaced with a notch filter 47 and a narrowband filter 57 (corresponding to the artificial beacon wavelength λ).
[0100] The working principle of this embodiment is briefly described as follows:
[0101] (1) Under t...
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