Abstract
This paper introduces advanced frameworks to enhance the performance of electric multirotors for Urban Air Mobility (UAM) applications. Key contributions include the battery State-of-Energy (SOE) estimation model, which is based on aerodynamics and momentum theory. Additionally, a discrete-time state-space framework integrates vehicle dynamics with SOE, refined using an Extended Kalman Filter (EKF). Furthermore, an algorithm and a Model Predictive Control (MPC) method are introduced to enhance energy efficiency during horizontal forward flight trajectory (Cruise Phase). These approaches utilize inertia-preserved velocity to produce Impulse Horizontal Thrusts (IHT) rather than Continuous Horizontal Thrusts (CHT). Simulation results indicate approximately 26% energy savings achieved with these strategies, highlighting their potential to boost the efficiency and feasibility of UAM substantially.
| Original language | English |
|---|---|
| Article number | 126569 |
| Journal | Applied Energy |
| Volume | 401 |
| DOIs | |
| Publication status | Published - 15 Dec 2025 |
Bibliographical note
Publisher Copyright:© 2025 Elsevier Ltd
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
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SDG 11 Sustainable Cities and Communities
Keywords
- Battery modeling
- Electric multirotor aerial vehicle
- Extended Kalman filter (EKF)
- Impulse horizontal thrust (IHT)
- Inertia-preserved velocity
- Model predictive control (MPC)
- State of energy (SOE)
- Trajectory/energy management
- Urban air mobility (UAM)
- eVTOL
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