Real-time sun avoidance method of camera with cylindrical hood for geostationary orbit satellite
A geostationary orbit and sunshade technology, which is used in motor vehicles, space navigation equipment, space navigation aircraft, etc., can solve problems such as the inability to meet the needs of imaging tasks, eliminate hidden dangers of jet unloading, avoid a smooth process, and improve use safety. sexual effect
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[0051] The specific parameters of geostationary orbit satellites are as follows:
[0052] Avoidance parameters: sunlight avoidance safety angle α = 30°, Δ = 2.5° indicates the avoidance margin angle, a and b indicate parabolic coefficients, here select a = -6, b = 1.025.
[0053] Orbit initial value:
[0054] orbital epoch March 20, 2010 15:00:00,
[0055] Semi-major axis (km) 42164.238885703373,
[0056] Eccentricity 0.00013534077386388930,
[0057] Orbit inclination (degrees) 0.0026285532110204346,
[0058] Ascending node right ascension (degrees) 131.49687827859242,
[0059] Argument of perigee (degrees) 95.486669826235925,
[0060] Mean anomaly (degrees) 267.65066999183171.
[0061] Calculated according to the steps given earlier,
[0062] (1) According to the solar orbit coordinate So, the sun avoidance offset angle can be calculated in real time, for example, at the starting point of the sun avoidance,
[0063] So=[-0.537264370964670 0.000039568429893 0.84341389346...
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