The effectiveness of Individual Blade Control systems (IBC) to reduce N/rev vibrations (N = number of blades) and noise were already proofed by full-scale wind tunnel and flight tests. Due to the system architecture and the resulting blade-individual control capability other newer applications like Performance Improvement, In-Flight-Tracking & Balancing and Reconfiguration after partial loss of control system performance or blade damage can be addressed. The objective of the program NABIS was to provide evidence that IBC systems provide positive effects regarding these new applications by means of full-scale wind tunnel tests with an UH-60A rotor at the National Full Aerodynamics Complex (NFAC). Within the wind tunnel tests a special emphasis was laid on the development and applicability of closed loop control algorithms. For the specific and new application of In-Flight-Tracking and Balancing new electrical blade root control actuation systems adapted to the low bandwidth and low authority application should be developed and tested within a laboratory environment.