Mars atmospheric entry guidance for reference trajectory tracking based on robust nonlinear compound controller
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DOI: 10.1016/j.actaastro.2016.12.013
Abstract: Abstract A robust entry guidance law based on terminal sliding mode and second-order differentiator is designed for trajectory tracking in this paper. The bank angle is regarded as the control variable. A novel nonlinear compound… read more here.
Keywords: nonlinear compound; entry guidance; controller; trajectory tracking ... See more keywords