The nonlinear iterative closed loop configuration of control allocation for aircraft with multiple control effectors

Proceedings of the 26th Chinese Control Conference, CCC 2007

Volumn , Issue , 2007, Pages 755-757

  Yang, Lingyu ^a   Zhong, Youwu ^a   Shen, Gongzhang ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Aircraft with multiple control effectors; Control allocation; Flight control; Iterate

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; END EFFECTORS; ERROR ANALYSIS; ITERATIVE METHODS; NONLINEAR CONTROL SYSTEMS; ROBUST CONTROL;

AIRCRAFT WITH MULTIPLE CONTROL EFFECTORS; CONTROL ALLOCATION; LINEAR DESCRIPTION; NONLINEAR ITERATIVE METHODS;

FLIGHT CONTROL SYSTEMS;

EID: 37749043711     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/CHICC.2006.4347425     Document Type: Conference Paper

References (5)

1. James M Buffmgton. Tailless Aircraft Control Allocation, AIAA-97-3605, 1997.
2. Chinese source
3. Addington G A, Myatt. J H Control-Surface Deflection Effects on the Innovative Control Effectors (ICE 101) Design, AFRL-VA-WP-TR-2000-3027, 2000.
4. Chinese source
5. Chinese source