Journal
INTERNATIONAL JOURNAL OF AUTOMATION AND COMPUTING
Volume 8, Issue 1, Pages 122-127Publisher
SPRINGER HEIDELBERG
DOI: 10.1007/s11633-010-0563-z
Keywords
Integrated guidance and control; unmatched uncertainty; adaptive control; dynamic surface control; homing missiles
Funding
- National Natural Science Foundation of China [60710002, 60974044]
Ask authors/readers for more resources
Integrated guidance and control for homing missiles utilizing adaptive dynamic surface control approach is considered based on the three channels independence design idea. A time-varying integrated guidance and control model with unmatched uncertainties is first formulated for the pitch channel, and an adaptive dynamic surface control algorithm is further developed to deal with these unmatched uncertainties. It is proved that the proposed feedback controller can ensure not only the accuracy of target interception, but also the stability of the missile dynamics. Then, the same control approach is further applied to the control design of the yaw and roll channels. The 6-degree-of-freedom (6-DOF) nonlinear missile simulation results demonstrate the feasibility and advantage of the proposed integrated guidance and control design scheme.
Authors
I am an author on this paper
Click your name to claim this paper and add it to your profile.
Reviews
Recommended
No Data Available