The MCLAWS-2 initial gain set was determined by nonlinear piloted simulation and linear analysis.
Sources
- M. B. Tischler, C. L. Blanken, K. K. Cheung, S. S. M. Swei, V. Sahasrabudhe, and A. Faynberg, “Modernized Control Laws for UH-60 BLACK HAWK Optimization and Flight-Test Results,” Journal of Guidance, Control, and Dynamics, vol. 28, no. 5, pp. 964–978, Sep. 2005, doi: 10.2514/1.8021.
Backlinks
Gain Scheduling
[[MCLAWS-2]]
[[Nonlinear Flight Control Simulations]]