SBIR-STTR Award

Reconfigurable VTOL Energy Management System
Award last edited on: 3/27/2023

Sponsored Program
SBIR
Awarding Agency
NASA : GRC
Total Award Amount
$124,970
Award Phase
1
Solicitation Topic Code
A1.06
Principal Investigator
Brad E Paden

Company Information

Launchpoint Technologies LLC (AKA: Magnetic Moments~LaunchPoint Technologies Inc)

5735 Hollister Avenue Suite B
Goleta, CA 93117
   (805) 683-9659
   info@launchpnt.com
   www.launchpnt.com
Location: Multiple
Congr. District: 24
County: Santa Barbara

Phase I

Contract Number: 80NSSC18P1894
Start Date: 7/27/2018    Completed: 2/15/2019
Phase I year
2018
Phase I Amount
$124,970
This SBIR Phase I develops hardware and software for energy management in electric VTOL aircraft. It focuses on techniques to ensure short-time-scale stability in power micro-grids, and optimization-based control at somewhat longer (~10-100 ms) time-scales for propulsion system and vehicle control, which is managed by a vehicle Energy Management System (vEMS). Fast optimization and model-based decision making are key to the approach. Experiments will be conducted with a hybrid power plant consisting of an internal combustion engine, an iron-less dual-halbach-array starter motor/generator, and a new 6-phase regenerative motor drive. The project is organized into three Technical Objectives: TO #1: Reconfi gurable Component, Subsystem, and System Topology Models Reconfigurability is enabled at three levels in the vEMS-controlled system. At the component level, parametric models are used so that components in a new vehicle system or a faulted system can be configured with a parameter list. Subsystems are similarly configured. At the system level, the topology is reconfigurable because of technical conditions (incremental passivity) placed on each component to ensure that the assembled micro-grid is stable regardless of the interconnection. With stable short-time-scale dynamics, the vEMS uses component models to optimally manage interactions on the micro-grid. TO #2: Incremental Passivity with Application to a 1.5kW Regenerative Drive LaunchPoint proposes to design a 1.5kW regenerative drive for the 6-phase starter motor/generator such that it is incrementally passive as seen from the bus. TO #3: Real-Time Optimal Control for Energy Management The project will make use of a recently developed tool, named TensCalc, that generates specialized C-code for real-time decision and control with up to a few thousand optimization variables/constraints. This fast optimization tool will be at the heart of the vEMS system and enable millisecond time-scale decision making. Potential NASA Applications This project relates to NASAs efforts in electric and hybrid-electric flight, urban air mobility (UAM) and research in power electronics. NASA vehicles and concepts related to this work are the X-57, GL-10, and SUGAR Volt. Potential Non-NASA Applications The US Department of Defense and number of companies are developing or have interest in electric and hybrid-electric flight. Commercial entities include Uber, Amazon, Vayu, Elroy Air, Martin Aerospace, Boeing, and numerous others.

Phase II

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Start Date: 00/00/00    Completed: 00/00/00
Phase II year
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