New Theoretical And Experimental Studies On Spacecraft Attitude Determination Using Star Sensors
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Accurate and Efficient Algorithms for Star Sensor Based Micro-Satellite Attitude and Attitude Rate Estimation
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Development Of Gyroless Attitude And Angular Rate Estimation For Satellites
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Vutukuri, SrianishThe halo orbits around the Sun-Earth L1 Lagrange point form an ideal location for deploying a solar observation spacecraft as they offer uninterrupted, long-duration visibility of the Sun. However, the complex orbital and ...

