Integrated Damage-Adaptive Control System (IDACS), Phase II

SSCI proposes to further develop, implement and test the damage-adaptive control algorithms developed in Phase I within the framework of an Integrated Damage Modeling & Adaptive Control (IDMAC) system. The proposed IDMAC system design will be based on the following: (i) Development of a coupled structural and aerodynamic model of aircraft dynamics under structural damage, (ii) Generation of a set of models describing different damage cases; (iii) Model set reduction to arrive at a reduced set of control design models; and (iv) Use of the reduced model set to design multiple-model stochastic damage estimators and corresponding reconfigurable controllers to stabilize the aircraft and achieve acceptable performance of the closed-loop flight control system. The proposed IDMAC system will be tested on transport aircraft models selected in consultation with NASA Langley.

Potential NASA Commercial Applications: Potential non-NASA applications of the IDMAC system are in the area of commercial and military aircraft. Autonomous IDMAC will also find wide applications in other programs such as spacecraft control and Unmanned Aerial Vehicles (UAV).

This is a mature technology (TRL 7+) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.

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