| 摘要 |
<p>The invention relates to a laser terminal (10) intended for being installed on-board an aircraft (2), the laser terminal (10) comprising: a frame having a plurality of openings (Oi) and including a first portion (F1) which is adjustable such as to make it possible to direct a laser beam (B) according to a transmission direction (Dir); a performance-optimisation device including: an interface (Int) capable of receiving at least one aerodynamic parameter (P_ae); a processor (K) including a first function for determining a first set-point (C1) for pressure regulation according to the aerodynamic parameter (P_ae) and the direction of transmission (Dir) of the laser beam; means for local pressure regulation, in accordance with at least the first set-point (C1), in a first area next to the frame by means of at least one opening (Oi) allowing a circulation of a flow of a fluid.</p> |
