The Department of Defense (DOD) is seeking proposals for the development of a Distributed Acceleration Sensor for Integrated Flight and Structural Control. The objective is to create a low-cost, low-SWAP (size, weight, and power), embeddable measurement system that can measure real-time structural acceleration of an airborne platform's mode shapes. This technology will enable tightly integrated flight and aeroelastic control on future platforms, enhancing their speed, endurance, and agility.
Currently, conventional accelerometers can measure accelerations at distinct points, but they require a priori knowledge of the mode shapes. Fiber optic sensors can provide distributed measurements of structural displacement, but they lag acceleration by 180 degrees, posing stability challenges for aircraft control. The goal of this SBIR topic is to develop sensors and electronics that can produce real-time acceleration measurements of airframe structural modes without the need for a priori knowledge.
The proposed sensor should intrinsically measure structural acceleration for spans greater than 40 feet and exploit material phenomena that correlate to structural accelerations. The project will involve conceptual design, modeling and simulation, fabrication and testing of a prototype sensor, and validation in a controlled laboratory environment. The precision, accuracy, range, drift, noise, and bandwidth of the sensor will be quantified, and potential air platforms for operational testing will be identified.
In Phase III, the sensor's potential for use in a structural and flight dynamic closed-loop feedback system will be assessed, enabling future tailless air platforms capable of high-speed dash, long-endurance loiter, and agile maneuvering. Additionally, the sensor's application in structural monitoring and condition-based maintenance in commercial civil and aerospace engineering firms will be explored.
The project duration will include Phase I, which involves producing a conceptual design and estimating the cost of building and testing a prototype, Phase II, which includes fabricating and testing the prototype sensor, and Phase III, which focuses on dual-use applications and collaboration with DoD air platform providers and commercial firms. The solicitation is open until June 12, 2024, and more information can be found on the DOD SBIR website.