| 摘要 |
The invention concerns a method for piloting a craft steerable by means of an actuator, servocontrolled in attitude on a trajectory and subjected to external perturbations which consists, at least in pitch, in first defining a piloting law including a first order correcting term, a transfer term comprising parameters characteristic of the craft and of the external perturbations (A6, K1), a gain in attitude (Kp) and a gain in attitude speed (Kv); and relationships correlating the attitude speed gain and the parameters of the correcting term based in particular on attitude gain and on terms representing rapidity ( omega n) and damping ( zeta ) instructions, and for at least one phase of the craft flight, in selecting the attitude gain and the rapidity and damping terms and deducing therefrom the parameters of the correcting term and the speed gain of the piloting law. |
