The required lateral maneuver trajectory on equilibriumglide assumption is specified according to the designed angles of attack and bank.
根据所设计的攻角和倾侧角,即可实现平衡滑翔情况下预定机动模式的侧向机动。
2
Based on the flight corridor and equilibriumglide assumption, we can determine the angle-of-attack that satisfies the lateral weaving maneuver and all the flight constraints.