高超声速飞行器新型攻角约束反演控制

doi:10.12305/j.issn.1001-506X.2022.04.29

Abstract

Abstract:

For the control problem of hypersonic vehicle with angle of attack (AOA) constraint, a backstepping control scheme combining constrained command filter and prescribed performance method is proposed. Firstly, the altitude subsystem is divided from the hypersonic vehicle motion model and the controller is designed based on the backstepping control method. In order to solve the problem of AOA constraint, a constrained command filter is constructed to limit the virtual command of AOA and ensure the virtual command's differentiability. Then, the constraint range is set in advance by using the prescribed performance method to ensure that the tracking error of AOA meets the constraint condition and to improve its transient and steady performance. In addition, linear extended state observer (LESO) is used to observe and compensate the parameter uncertainties of the system and external disturbances. Based on Lyapunov stability theory, it is proved that the tracking error of the system is uniformly bounded. Finally, the simulation results show that the proposed method is effectiveness.

Key words: hypersonic vehicle, angle of attack (AOA) constraint, command filter, prescribed performance, linear extended state observer

CLC Number:

V249.1

Junbao WEI, Haiyan LI, Jing LI. Novel backstepping control for hypersonic vehicle with angle of attack constraint[J]. Systems Engineering and Electronics, 2022, 44(4): 1310-1317.

Figures/Tables 9

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References 23

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符号	取值	符号	取值
m/(lb/ft)	300	C_D^α/rad^-1	-4.531 5
I_yy/(lb·ft)	5×10⁵	C_D⁰	-0.045 315
ρ/(slug/ft³)	6.742 9×10^-5	C_L^α/rad^-1	4.677 3
g/(ft/s²)	32.17	C_L⁰	-0.018 714
S/ft²	17	C_M^α²/rad^-2	6.292 6
$\bar{c}$/ft	17	C_M^α/rad^-1	2.133 56
z_T/ft	17	C_M⁰	-0.189 79
C_D^α²/rad^-2	5.822 4	C_M^δ_g/rad^-1	-1.289 7

参数	取值	参数	取值
k_h	0.5	ω_γ	10
k′_h	0.5	ω_α	10
k_γ	1	ω_q	20
k_α	2	μ	0.5
σ_α	0.001	$\tilde \omega $₀	0.01
k_q	1	$\tilde \omega $_∞	0.005
ξ_γ	0.5	ω_γ0	5
ξ_α	1	ω_q0	5
ξ_q	0.5	—	—

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Novel backstepping control for hypersonic vehicle with angle of attack constraint

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