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Published byWesley Walker Modified over 8 years ago
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Satellite Altimetry
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The range R from satellite to mean sea level is estimated by
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Past Missions
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Current Missions
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Radar Measurement principles
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Normalized radar Cross Section
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Ocean Surface Reflectivity
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Atmospheric Attenuation Clear Sky Transmittance at normal incidence angle
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Cloud Attenuation
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Rain Attenuation
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Two-Way Travel Time Pulse-Limited
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Average Returned Waveform
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Fig 16: Average of 1, 25, and 1000 Simulated Independent time series of illuminated area
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Instrument Corrections Doppler Shift Altimeter Acceleration Error Oscillator Drift Error Pointing angle and sea-state correction
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Foot Print Size
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Range Estimation 1cm accuracy from satellite altimetry by measuring two-way travel time is a big challenge due to the reasons: Atmospheric Effects: Dry Tropospheric Refraction Wet Tropospheric Refraction Ionospheric Refraction Sea-State Effects: Electromagnetic Bias Skewness Bias
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TECU estimated from Dual-freq measurements
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Orbit Determination
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