SBIR/STTR Research Award

Real Time Flight Envelope Estimation and Feedback for UAS Verification, Validation, and Certification

Award identifier 46114927c6fb1d4138731414e53d30e28eef81eedb9ca348ce7165e25f0b2685Awarding agency National Aeronautics and Space Administration

Award amount

$117,974

Program and phase

SBIR · Phase I

Award year

2019

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
BOLDER FLIGHT SYSTEMS INC
Proposal award date
2019-08-19
Contract end date
2020-02-18
UEI
EJHETYKGGGN5
Solicitation number
SBIR_19_P1
Topic code
A2

Research abstract

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.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

8 SBIR/STTR records share this UEI (2019–2025). Reported award amounts total $3,453,410. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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