Relative kinematics for a jerk-level trajectory generation system

Abstract Using electric vertical takeoff and landing (eVTOL) aircraft for urban air mobility requires a high level of maneuverability and tracking accuracy from the flight guidance systems. This can be achieved by constructing a high-order desired trajectory, in order to provide jerk-level feedforward commands and acceleration-level relative kinematics. In this paper, we perform a noise analysis on a trajectory system where relative kinematics are computed numerically, and we show the resulting noise effects. We then present an analytical alternative which improves the noise sensitivity. Additionally, we develop a smoothing strategy for obtaining a high-order parametrization of a trajectory designed with low-order clothoid curves. The methods presented in the paper are tested and validated in closed-loop simulations and through flight tests on a 700 kg medical-evacuation eVTOL aircraft. The results of these tests are presented and discussed.

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Publication Details

Journal
CEAS Aeronautical Journal
Published
2025-06-28
DOI
https://doi.org/10.1007/s13272-025-00861-y
Primary Topic
Robotic Mechanisms and Dynamics
Type
article
Field-Weighted Citation Impact
0.00

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article

Relative kinematics for a jerk-level trajectory generation system

Dominik Heimsch, Agnes Steinert, Hugh H. T. Liu, Florian Holzapfel et al.
CEAS Aeronautical Journal
Robotic Mechanisms and Dynamics
article

Relative kinematics for a jerk-level trajectory generation system

Dominik Heimsch, Agnes Steinert, Hugh H. T. Liu, Florian Holzapfel, Zoe Mbikayi, Philippe Rudolph
article en

Abstract

Abstract Using electric vertical takeoff and landing (eVTOL) aircraft for urban air mobility requires a high level of maneuverability and tracking accuracy from the flight guidance systems. This can be achieved by constructing a high-order desired trajectory, in order to provide jerk-level feedforward commands and acceleration-level relative kinematics. In this paper, we perform a noise analysis on a trajectory system where relative kinematics are computed numerically, and we show the resulting noise effects. We then present an analytical alternative which improves the noise sensitivity. Additionally, we develop a smoothing strategy for obtaining a high-order parametrization of a trajectory designed with low-order clothoid curves. The methods presented in the paper are tested and validated in closed-loop simulations and through flight tests on a 700 kg medical-evacuation eVTOL aircraft. The results of these tests are presented and discussed.

CEAS Aeronautical Journal
University of Toronto (CA), Toronto Rehabilitation Institute (CA), Technical University of Munich (DE)
Technische Universität München
Openalex Percentile: Top 83%
Robotic Mechanisms and Dynamics
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