NASA SBIR 2015 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 15-1 S3.04-9554
SUBTOPIC TITLE: Unmanned Aircraft and Sounding Rocket Technologies
PROPOSAL TITLE: Optimization Of Fuel Consumption Using Atmospheric Vertical Air Currents

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Dynsan, LLC
8000 Madison Boulevard, Suite D102 PMB303
Madison, AL 35758 - 2055
(256) 468-6458

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr Jean-Jacques Malosse
jjm@dynsan.com
8000 Madison Blvd. STE-D102 PMB303
Madison, AL 35758 - 2055
(256) 468-6458

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Maciej Z. Pindera
mzp@dynsan.com
8000 Madison Blvd. STE-D102 PMB303
Madison, AL 35758 - 2055
(256) 468-6458

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 2
End: 4

Technology Available (TAV) Subtopics
Unmanned Aircraft and Sounding Rocket Technologies is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?
No

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
DynSan proposes to develop a flight controller that will preserve the aircraft trajectory while directing to sources of potential updrafts to optimize fuel consumption of Unmanned Aircraft Vehicles (UAV). Fuel consumption represents a significant factor in powered flight operations; it is desirable therefore to limit the fuel consumption in order to extend an aircraft's flight range and/or flight duration. Glider pilots use their knowledge in micrometeorology to locate and exploit sources of lift. The same soaring techniques could be used with UAV, to exploit atmospheric energy that is renewable. The exploitation of this source of energy can be automated using a controller that will correct the aircraft trajectory in order to optimize the climb rate and thus the average cruising speed. Dynamic soaring is the final source of energy that exploits the differential wind velocity at different heights. In Phase I, we propose to build a map of potential updrafts based on terrain and meteorological conditions and test the validity of this map using actual data extracted from sailplane contests. The data will provide the horizontal and vertical glider speeds; using glider polars will allow us to extract information of the vertical movement of the surrounding airmass. This information will be used by a novel controller that will direct the UAV through locations or rising air, while keeping the aircraft on trajectory to target. The flight of a model UAV through selected topographic and atmospheric conditions will be simulated. Comparisons to actual archived flight data will be made. In Phase II, we will fabricate, program and integrate the developed controller on a real UAV. With the UAV equipped with cameras, it will be possible to visually locate the updraft columns that are marked by fair weather cumulus clouds and manually direct the UAV to such columns. The controller performance in optimizing the aircraft climb rate will then be tested.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
NASA will be able to develop novel UAVs that will exploit atmospheric features and increase the efficiency of these aircraft. Moreover NASA expressed a need for improving dropsondes. In order to explore more efficiently atmospheric features, these dropsondes need to be guided. The technology developed in this proposal can be applied to these devices.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The development of an autopilot optimizing the fuel consumption is of interest to the civilian and military market.

Usage of UAVs by military forces is rapidly accelerating. One of the advantages of unmanned systems is that they can be very light since they do not need to carry a pilot. When unmanned aircraft are piloted from the ground, the communication can be intercepted and the aircraft cannot remain stealthy. Therefore, it is desirable for a UAV to fly autonomously for the longest period of time. Our approach that allows the aircraft to fly autonomously for extended periods of time has strong support from Boeing and Lockheed-Martin (see letters of support at end of proposal) and can be used with their fleet of vehicles such as the K-MAX, Desert Hawk III, Sky Spirit, SURGE-V, EER, Samurai, and Nighthawk Micro UAVs.

TECHNOLOGY TAXONOMY MAPPING (NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.)
Ad-Hoc Networks (see also Sensors)
Aerodynamics
Algorithms/Control Software & Systems (see also Autonomous Systems)
Analytical Methods
Atmospheric Propulsion
Autonomous Control (see also Control & Monitoring)
Models & Simulations (see also Testing & Evaluation)
Sources (Renewable, Nonrenewable)
Vehicles (see also Autonomous Systems)
Verification/Validation Tools

Form Generated on 04-23-15 15:37