TY - GEN
T1 - Active coning compensation for control of spinning flying vehicles
AU - Salman, Mishah Uzziél
AU - Chang, Borchin
PY - 2010
Y1 - 2010
N2 - Many gun launched projectiles spin to maintain in-flight dynamic stability. This spinning often induces the gyroscopic phenomenon known as precession, or coning. Coning poses a problem for actively controlling the projectile. A control scheme is proposed that can compensate for the coning angle of the projectile and allow front-mounted canards to efficiently change the projectile flight path without reaching a stall condition. Closed-loop regulation and H2 control theories are employed to construct the controller.
AB - Many gun launched projectiles spin to maintain in-flight dynamic stability. This spinning often induces the gyroscopic phenomenon known as precession, or coning. Coning poses a problem for actively controlling the projectile. A control scheme is proposed that can compensate for the coning angle of the projectile and allow front-mounted canards to efficiently change the projectile flight path without reaching a stall condition. Closed-loop regulation and H2 control theories are employed to construct the controller.
UR - http://www.scopus.com/inward/record.url?scp=78649434891&partnerID=8YFLogxK
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U2 - 10.1109/CCA.2010.5611245
DO - 10.1109/CCA.2010.5611245
M3 - Conference contribution
AN - SCOPUS:78649434891
SN - 9781424453627
T3 - Proceedings of the IEEE International Conference on Control Applications
SP - 1832
EP - 1837
BT - 2010 IEEE International Conference on Control Applications, CCA 2010
T2 - 2010 IEEE International Conference on Control Applications, CCA 2010
Y2 - 8 September 2010 through 10 September 2010
ER -