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Robust spline-line energy management guidance algorithm with multiple constraints and uncertainties for solid rocket ascending
作者姓名:Songyan WANG  Fei LIU  Tao CHAO  Ming YANG
作者单位:Control and Simulation Center,Harbin Institute of Technology,Harbin 150001,China
基金项目:supported by th National Natural Science Foundation of China (Nos. 61627810, 61790562 and 61403096);
摘    要:For the solid rocket with depletion shutdown system, effective energy management is significant to meet terminal constraints by exhausting excess energy. Several traditional energy management algorithms cannot satisfy the altitude constraint and path constraints are not sufficiently considered. The velocity adjustment capability of these algorithms is limited and the uncertainties are not considered. Based on the on-line programming of velocity capability curve, Spline-Line Energy Management(SLE...

收稿时间:30 September 2020

Robust spline-line energy management guidance algorithm with multiple constraints and uncertainties for solid rocket ascending
Songyan WANG,Fei LIU,Tao CHAO,Ming YANG.Robust spline-line energy management guidance algorithm with multiple constraints and uncertainties for solid rocket ascending[J].Chinese Journal of Aeronautics,2022,35(2):214-234.
Authors:Songyan WANG  Fei LIU  Tao CHAO  Ming YANG
Institution:Control and Simulation Center, Harbin Institute of Technology, Harbin 150001, China
Abstract:For the solid rocket with depletion shutdown system,effective energy management is sig-nificant to meet terminal constraints by exhausting excess energy.Several traditional energy man-agement algorithms cannot satisfy the altitude constraint and path constraints are not sufficiently considered.The velocity adjustment capability of these algorithms is limited and the uncertainties are not considered.Based on the on-line programming of velocity capability curve,Spline-Line Energy Management (SLEM) guidance algorithm is proposed.It introduces lateral maneuvers to further consume the available velocity on the basis of longitudinal energy management.After expressing the constraints as several algebraic equations,the closed-loop guidance problem is con-verted to solving a system of nonlinear equations about the curve parameters in real time.The advantage is that the altitude constraint can be satisfied theoretically.The overload and control variable change rate and amplitude constraints are also considered during the flight by constructing the feasible boundary of velocity capability curve.To improve the robustness,it is further extended by estimating the actual uncertainties.The effectiveness and advantages of SLEM are demonstrated by simulations and comparisons with other energy management algorithms.Simulation results show that the proposed approach can satisfy multiple constraints with high precision under the con-dition of uncertainties.
Keywords:Ascent guidance  Energy management  Multiple constraints  Solid rockets  Uncertainty  Velocity capability curve
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