Multi-input, multi-output flight control system design for the YF-16 using nonlinear QFT and pilot compensation
Russel B. Miller, Isaac M. Horowitz, Constantine H. Houpis, A. Finley BarfieldVolume:
4
Year:
1994
Language:
english
Pages:
20
DOI:
10.1002/rnc.4590040112
File:
PDF, 1.11 MB
english, 1994