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Our Mission

At MLB Company, our mission is to provide our customers with the most cost effective solutions to accessing aerial information. We specialize in the research and development, manufacturing and training of complete Unmanned Aerial Systems (UAS) and aerial imaging serices utilizing our UAS products. Our products include the low cost and portable Bat-3 UAV equipped with a gimbal camera which allows for live video streaming, and the innovative vertical-take-off-and-land (VOTL) V-Bat that combines the ability to hover with the efficiency of high speed horizontal flight.

MLB Company is also highly involved in research consultating that continuously brings innovation to aircraft design and aerial image processing. Here at MLB Company, we look forward to future partnerships with you in your aerial ventures.

Vertical Takeoff and Landing aircraft
A Quiet diesel powered hand launched aircraft with autopilot (wing leveling and altitude hold) and 1 mile range (telemetry limited). Speed 15-40 mph.
Aircraft was built and operated for NASA Ames Research Center in 2001. Fully autonomous operation was achieved from San Francisco Bay. With the addition of fixed undercarriage, the airplane was also operated at Moffett Field.

VolcanoThe Volcano aircraft is designed to carry a 15 lb payload over 750 miles and up to an altitude of 12000 ft.

Cooperative project with UC-Berkeley and the US Marine Corps.
The trochoidal wing planform has only 11% less area than a circular wing for a given size, yet has the desirable aerodynamic properties of a delta wing planform because its size normal to the flow direction increases along the wing centerline.
Fully autonomous small ducted-fan hovering vehicle.
Mini-UAVs for Convoy Protection (700 KB). This article was the cover feature for the May/June 2004 edition of Unmanned Systems magazine.

Autonomous Robots in SWAT Applications: Research, Design, and Operations Challenges (220 Kb). MLB worked with the Mountain View/Palo Alto Regional SWAT Team to identify current and future roles of UAVs and other autonomous vehicles in the SWAT environment.

Integrated Aerodynamics and Control System Design for Tailless Aircraft (7.5 MB). This paper presents a numerical method for simultaneously designing an aircraft and its feedback control system to minimize drag with a fixed level of handling qualities.

Flight Tests of an Oblique Flying Wing Small Scale Demonstrator (3.2 MB). This paper summarizes the results of analytical and experimental work on oblique all-wing stability and control issues, including results from the flight test of a 20 foot span, 80 pound demonstrator model with an onboard computer stabilization system.

Design and Flight Test Results for Micro-Sized Fixed-Wing and VTOL Aircraft (87 Kb). This paper studies the importance of aerodynamics, propulsion, and mission requirements on the design of a mAV. A Multi-Disciplinary Optimization method is used to size mAV’s for a baseline mission.

Design of Micro Air Vehicles and Flight Test Validation (0.8 MB). Flight control, sensing, communication and propulsion have the strongest impact on mission performance.