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Stochastic Model Predictive Control for Airspeed Optimization Using Successive Convexification

机译:基于连续凸化的空速优化随机模型预测控制

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The present paper addresses the problem of airspeed profile optimization along a pre-assigned trajectory and newly proposes a real-time method for robust airspeed planning under uncertainties of wind forecasts and the response time of the lower-level closed-loop system of the airspeed control. In order to reduce the number of decision variables of the airspeed profile optimization, the method proposed herein adopts the stochastic model predictive control (MPC) based on the unscented transform (IT) for uncertainty modeling. In addition, to make each step of the MPC tractable, we apply successive convexification of the non-convex constraints incurred by the IT via local linearizations and relaxations to convex quadratic inequalities. Through numerical simulations, the effectiveness of the proposed approach is confirmed in terms of the fuel efficiency, punctuality of the arrival, low pilot workload, and high computational speed.
机译:本文涉及沿预先分配的轨迹的空速轮廓优化问题,并且新提出了一种在风预测的不确定性下的鲁棒空速规划的实时方法,以及空速控制的较低级闭环系统的响应时间。为了减少空速轮廓优化的判定变量的数量,本文提出的方法基于未精确的变换(IT)来采用随机模型预测控制(MPC)以进行不确定性建模。此外,为了制造MPC易诊断的每个步骤,我们通过局部线性化和放松来应用IT引起的非凸的约束的连续凸起,以凸起二次不等式。通过数值模拟,在燃油效率,到达的准时,低试点工作量和高计算速度方面确认了所提出的方法的有效性。

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