Optical device for wide waveband plane grating dispersion type imaging spectrometer
A technology of imaging spectrometer and planar grating, which is applied in the field of imaging spectrometer, can solve the problems of large residual aberration and large astigmatism, and achieve the effects of wide spectral range, cost reduction and good imaging quality
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[0011] Specific implementation mode one, combination figure 1 with figure 2 In this embodiment, the optical device of a wide-band plane grating dispersive imaging spectrometer is described. The device includes a front optical system and a Czerny-Turner spectral imaging system, and the front optical system includes an aperture stop 1 and an off-axis parabolic mirror 2; The Czerny-Turner spectral imaging system is composed of an entrance slit 3, a spherical collimator 4, a plane grating, a plane mirror, a toroidal focusing mirror, and an area array focal plane detector; the entrance slit 3 is located by the aperture stop On the focal plane of the front optical system composed of 1 and off-axis parabolic mirror 2, the light exiting through the incident slit 3 is projected onto the spherical collimator 4, collimated by the spherical collimator 4, and then projected onto the plane grating 5 , The diffracted light emitted from the plane grating 5 is deflected by the plane mirror 6 an...
Example Embodiment
[0012] Specific implementation mode two, combination figure 2 with image 3 As shown, this embodiment is an example of the optical device of the wide-band planar grating dispersive imaging spectrometer described in the first embodiment, including a front optical system composed of an aperture stop 1 and an off-axis parabolic mirror 2 and an A spectral imaging system composed of slit 3, spherical collimator 4, plane grating 5, plane mirror 6, toroidal focusing mirror 7 and area array focal plane detector 8.
[0013] The device of the invention is mounted on a satellite platform to detect ground targets, and the working waveband is 350nm-750nm. Combining 3, the X direction is the cross-orbit direction, which is the length of the incident slit 3, the Y direction is the satellite travel direction, which is the width of the incident slit 3, and the Z direction is the height of the satellite; the X direction corresponds to the ground width 25km, the satellite orbit height is 800km.
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