Picard mapping enforces integral constraints on parameterized ODE solutions to enable gradient-based estimation of 4-CMG inertia tensors and 28 F/A-18 control surface coefficients from sampled outputs.
A comparative study of real-time aircraft parameter identification schemes applied to NASA F/A-18 HARV flight data
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Picard Iteration for Parameter Estimation in Nonlinear Dynamic Models of Aircraft and Spacecraft
Picard mapping enforces integral constraints on parameterized ODE solutions to enable gradient-based estimation of 4-CMG inertia tensors and 28 F/A-18 control surface coefficients from sampled outputs.