部分约束下空中目标拦截制导控制一体化方法

doi:10.12305/j.issn.1001-506X.2023.04.22

Abstract

Abstract:

An integrated guidance and control (IGC) method with impact angle is proposed to intercept aerial target, constraints including input saturation and angle of attack are considered as well. Firstly, system with lumped uncertainties is modeled in pitch plane. Based on backstepping and command filter, constraints of impact angle and input saturation due to mechanical limitation of actuator are solved, signals with integration of error are constructed to handle with tracking errors. To guarantee the angle of attack within a predefined interval, barrier Lyapunov function is introduced. Based on Lyapunov theorem, stability of closed system, boundness of signals, and required constraints are proved. Numerical simulations exhibit effectiveness of interception with predefined impact angle for aerial target, constraints satisfied including input saturation and angle of attack, strong robustness also possessed of the method.

Key words: integrated guidance and control (IGC), impact angle, input saturation, state constraint, command filter

CLC Number:

V448.13

Lecheng LIANG, Bin ZHAO, Jun ZHOU, Wanli ZHAO. Integrated guidance and control method against aerial target with partial constraints[J]. Systems Engineering and Electronics, 2023, 45(4): 1134-1143.

Figures/Tables 18

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导弹参数	数值	导弹参数	数值
θ_M(0)/(°)	10	V_M/(m·s^-1)	500
θ_T(0)/(°)	180	V_T/(m·s^-1)	200
x(0)/m	8 000	y(0)/m	6 000

参数	数值	参数	数值	观测器参数	数值
k₁	0.2	k₃	25	b₁, b₃, b₅	300
k₂	10	β₁	1.2	b₂, b₄, b₆	600
τ₂	0.06	β₃	20

仿真条件	脱靶量/m	飞行时间/s
λ_d=30°	0.066 7	15.003
λ_d=60°	0.071 3	15.166
λ_d=90°	0.091 6	16.042

来源	参数	拉偏量/%
结构参数	m, S, L, J_z	±20
气动参数	c_y^α, c_y^z^δ, m_z^α, m_z^z^δ, m_z^ω_z	±20

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Integrated guidance and control method against aerial target with partial constraints

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