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Deterministic and Recursive Approach in Attitude Determination for InnoSAT

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Figure 1. InnoSat
Table 1. Inertial property of InnoSAT Parameters
Figure 2. Estimated Yaw( )ψattitude and error using QUEST and nonlinear dynamic EKF
Table 5. Accuracy analysis of EKF for nonlinear and linear model without eclipse Max Error Mean Error Max Mean
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Deterministic and Recursive Approach in Attitude Determination for InnoSAT

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