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Trajectory Generation Based on Power for Urban Air MobilityA method of generating trajectories based on power is proposed for Urban Air Taxis. The method is simpler and more direct than traditional methods because it does not require a detailed aircraft model or a flight control model. Instead, it allows the user to specify the route, the static longitudinal profile (altitude as a function of distance), and a power model to determine the progress in time along that profile. The power model can be determined from a recorded or simulated trajectory of the same aircraft type. This capability allows a trajectory to be generated or reshaped to avoid conflicts while preserving the basic performance characteristics. Net or excess power is defined as the rate of change of mechanical (kinetic and potential) energy, and it is modeled as a function of airspeed. The time steps between discrete points in space along the trajectory are used to yield a specified power as a function of airspeed, and they are determined by solving a cubic polynomial at each point. An elliptical profile is used to generate an example trajectory. The dependence of trip flight time on various parameters is analyzed and plotted.
Document ID
20250005340
Acquisition Source
Ames Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Russell A Paielli
(Ames Research Center Mountain View, California, United States)
Date Acquired
May 21, 2025
Publication Date
October 10, 2023
Publication Information
Publication: Frontiers in Aerospace Engineering
Publisher: Frontiers Media
Volume: 2
e-ISSN: 2813-2831
Subject Category
Air Transportation And Safety
Funding Number(s)
PROJECT: 629660
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
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