The required lateral maneuver trajectory on equilibrium glide 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。
Based on the flight corridor and equilibrium glide assumption, we can determine the angle-of-attack that satisfies the lateral weaving maneuver and all the flight constraints.
在此基础上，设计了平衡滑翔情况下满足侧向摆动式机动及飞行约束所需的攻角变化规律。
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