BOLDER FLIGHT SYSTEMS INC — National Aeronautics and Space Administration SBIR Phase I: A2

BOLDER FLIGHT SYSTEMS INC — SBIR Phase I award from National Aeronautics and Space Administration.

Amount
$117,974
Agency
National Aeronautics and Space Administration
Program / Phase
SBIR · Phase I
Topic
A2
Solicitation
SBIR_19_P1
NAICS
Place of performance
MN
Period
2019-08-19 → 2020-02-18

Description

Recent advances in computing enable Unmanned Aircraft Systems (UAS) to conduct high quality missions with the implicit promise of lower cost and effort than manned aircraft. However, a lack of methods, architectures, and tools to enable verification, validation, and certification of UAS flight control systems is a major technological barrier to widespread adoption of UAS in civil aviation and NASA research.Our innovation, Safety Assurance through Flight envelope Estimation in Real-time (SAFER), establishes trust through real-time estimation of safe and robust flight envelope boundaries and providing feedback and command limiting to keep the UAS within those boundaries. We propose to estimate these boundaries with an independent hardware module, requiring only effector commands as input, and enablingnbsp;any UAS to meet verification, validation, and certification requirements.Internally, our system will consist of an Inertial Measurement Unit, Global Navigation Satellite System receiver, and a processor. A cascaded set of Extended Kalman Filters will estimate inertial and synthetic air data states from IMU and GNSS data. Real-time identification and estimation methods will use these states to identify and estimate highly accurate and globally valid aircraft models, which will be used to estimate flight envelope boundaries and flight control system stability margins. Stability margins will be projected to the flight envelope boundaries to identify the envelope with adequate stability margins. Effector command limiting and feedback will be provided to keep the UAS within the stable and robust flight envelope boundaries.Phase I will establish feasibility through developing a prototype system and testing in simulation and flight test. Phase II is expected to mature the technologies and integrate low risk components. With an independent estimator of states, stability, and flight envelope boundaries, many potential applications exist within civil aviation and NASA research.