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Feature linear acceleration transition #642

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Feature linear acceleration transition #642

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@rachealerhard rachealerhard commented Jan 29, 2023 •
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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.

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coveralls commented Jan 29, 2023 •
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Coverage Status

Coverage: 90.298% (+0.02%) from 90.28% when pulling 76ba05d on feature-linear_acceleration_transition into f551a68 on develop.

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