SBIR/STTR Research Award

Integrated Flight Control Design and Multidisciplinary Optimization

Award identifier 3746e5b51ca73259ef8da2b87a4133b4f6b357303a56d4b89ad9ef25140e81c7Awarding agency National Aeronautics and Space Administration

Award amount

$124,952

Program and phase

SBIR · Phase I

Award year

2021

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
BECHAMO LLC
Proposal award date
2021-05-07
Contract end date
2021-11-19
UEI
Z272NRSJAMV4
Solicitation number
SBIR_21_P1
Topic code
A1

Research abstract

Multi-disciplinary optimization has emerged as a key technology required to make increasingly more sophisticated electric and hybrid-electric aircraft that require advanced CONOPS such as urban air mobility and distributed electric propulsion.nbsp; Current MDO design results may take into account many disciplines in the design resulting in an optimized aircraft, only to be locally re-optimized based on engineering performed post-aircraft configuration lock related to flight control, resulting in less efficient and less capable aircraft.Electric and hybrid-electric aircraft with distributed propulsion provide significant advantages such as significantly reduced stall speeds and dramatically increased power efficiency (gt;50%) (X-57).nbsp;nbsp; Software weighs nothing, so there always a push to move the problem downstream for controllers to manage in software, effectively trading bits for atoms.nbsp; The net result may be the control system requires faster than available actuation, inadequate control authority, or large feedback gains to stabilize unstable dynamics.nbsp; These issues are costly to uncover late in the system development, since typically flight controller work takes place after the configuration and outer-mode-line (OML) has been locked.nbsp;nbsp; It is essential to the success of hybrid and urban air mobility aircraft to include controllability of the aircraft within the aircraft optimization design.After decades of designing and flying flight controllers for new types of hybrid and distributed propulsion aircraft, our goal is to get add a controllability component to MDO to ensure the aircraft designed make the right trades and adjustments for flight controls.nbsp; Rather than throw a controller MDO cycle into the middle of the aircraft MDO, the controllability problem is broken down into a series of targeted hierarchical Components that contribute to the monolithic optimization suitable for the nonlinear and linear solvers in OpenMDO.nbsp;

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

2 SBIR/STTR records share this UEI (2021–2022). Reported award amounts total $924,572. Reported amounts are not federal obligations.

Phases: Phase II, Phase I

Agencies: National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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