Decoupling Control for the Actuator Dynamics of Spinning Missiles
When the missile rotates, there is a coupling problem caused by aerodynamic, inertial, and control cross-coupling in the pitch and yaw channels. This paper presents a dynamic precompensation diagonal dominance decoupling method for control coupling caused by the actuator dynamics. Firstly, the equiv...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2025-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/ijae/6653670 |