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Restrictions on unsteady gas dynamics working cycles supercomputer simulations due to accumulations of errors are developed.
The objective function calculation approaches of four circularity errors are developed and the initial population generation methods are given in order to save optimization time.
The implications of inconsistent geometric reference points, non-common time systems, and signal-specific range biases are analyzed, and strategies for coping with these issues in the definition and computation of SIS range errors are developed.
Another closely related work that deals with mobile asynchronous sensors is [12], where the estimation bounds with respect to both sensor synchronization and position errors are developed and validated by Monte Carlo simulations.
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The iterated logarithm law of estimation errors is developed.
The adjustment procedure for virtual pivot errors is developed by means of mathematical analysis.
A set of general altitude azimuth tracking angle formulas for a heliostat with a mirror-pivot offset and other geometrical errors were developed previously.
An algorithm to calculate the optimal orientation for minimizing flatness and cylindricity errors is developed and tested with the help of two test cases.
The conclusions were: Various sources of centroid estimation errors were developed.
Alternatively, a neural network model based on back propagation of errors was developed to assess the nonlinearity of the sought correlations between theoretical descriptors and experimental reaction barriers.
A framework for calculating carbon benefits by including assessment errors is developed.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com