Abstract
Recurrent finite memory and polynomial approximation are two techniques commonly used when one tackles a nonlinear estimation problem that includes space object and air and aircraft (AC) positioning and velocity vector component evaluation from angle-of-sight data provided by either an earth-based optoelectronic system or an AC-borne sighting system.
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References
Lantratov K (2002) Optical-electronic complex of outer space control “OKNO.” Cosmonautics Bull 3
Boguslavskiy JA, Egorova AV, Obrosov KV (1998) Aircraft instrument complex for autonomous information support of landing. Bull Russ Acad Sci Theor. Control Syst 2
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Boguslavskiy, J.A. (2016). Estimating Status Vectors from Sight Angles. In: Borodovsky, M. (eds) Dynamic Systems Models. Springer, Cham. https://doi.org/10.1007/978-3-319-04036-3_6
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DOI: https://doi.org/10.1007/978-3-319-04036-3_6
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