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Focuses on study which utilized the structured model reference adaptive control (SMARC) method for the active suppression of limit cycle oscillations for a typical wing section with a structural nonlinearity. Investigation on nonlinear aeroelastic control; Steps in adaptive feedback linearization; Advantages of SMARC over conventional adaptive methods.

We are developing an autonomous mobile robotic system to emulate six degree of freedom relative spacecraft motion during proximity operations. A mobile omni-directional base robot provides x, y, and yaw planar motion with moderate accuracy through six independently driven motors. With a six degree of freedom micro-positioning Stewart platform on top of the moving base, six degree of freedom spacecraft motion can be emulated with high accuracy. This paper presents our approach to dynamic modeling, control, and simulation for the overall system. Compared with other simulations that introduced significant simplifications, we believe that our rigorous modeling approach is crucial for the high fidelity hardware in-the-loop emulation. [ABSTRACT FROM AUTHOR]