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suavecode / SUAVE

An Aircraft Design Toolbox
suave.stanford.edu
GNU Lesser General Public License v2.1
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Feature linear acceleration transition #642

Open rachealerhard opened 1 year ago

rachealerhard commented 1 year ago

This PR adds a new mission segment for eVTOL transition. This is a linear acceleration, constant pitch rate, constant altitude segment.

The assumption of linear numerics is required to solve the matrix inversion for the control point velocities with a constant delta time step.

coveralls commented 1 year ago

Coverage Status

Coverage: 90.298% (+0.02%) from 90.28% when pulling 76ba05d3265027c53b3240688e4bacb1127d5712 on feature-linear_acceleration_transition into f551a684812cce532752a211e8da2cc89960d401 on develop.