NASA SBIR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- A1.06-4083
SUBTOPIC TITLE:
 Vertical Lift Technology and Urban Air Mobility
PROPOSAL TITLE:
 Reconfigurable VTOL Energy Management System
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
LaunchPoint Technologies, Inc.
5735 Hollister Avenue, Suite B
Goleta , CA 93117-6410
(805) 683-9659

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Bradley Paden
grants@launchpnt.com
5735 Hollister Avenue, Suite B Goleta, CA 93117 - 6410
(805) 683-9659

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Vicki Young
vyoung@launchpnt.com
5735 Hollister Avenue, Suite B Goleta, CA 93117 - 6410
(805) 683-9659
Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 6
Technical Abstract

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.


Form Generated on 05/25/2018 11:27:08