TY - GEN
T1 - Controller design for the F-14 pitch axis control problem using the quantitative feedback theory approach
AU - Yang, Jiann Shiou
PY - 1991/1/1
Y1 - 1991/1/1
N2 - The controller design of the F-14 pitch axis control problem is examined. The system block diagram is modified by using two, instead of the original four, controllers. The quantitative feedback theory (QFT) is then used to design the robust controllers. Simulations show that the angle-of-attack and pitch rate step responses of the designed system under the linearized plant parameter variations satisfy the design specifications.
AB - The controller design of the F-14 pitch axis control problem is examined. The system block diagram is modified by using two, instead of the original four, controllers. The quantitative feedback theory (QFT) is then used to design the robust controllers. Simulations show that the angle-of-attack and pitch rate step responses of the designed system under the linearized plant parameter variations satisfy the design specifications.
UR - http://www.scopus.com/inward/record.url?scp=0026401136&partnerID=8YFLogxK
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U2 - 10.23919/acc.1991.4791491
DO - 10.23919/acc.1991.4791491
M3 - Conference contribution
AN - SCOPUS:0026401136
SN - 0879425652
SN - 9780879425654
T3 - Proceedings of the American Control Conference
SP - 846
EP - 847
BT - Proceedings of the American Control Conference
PB - Publ by American Automatic Control Council
T2 - Proceedings of the 1991 American Control Conference
Y2 - 26 June 1991 through 28 June 1991
ER -