基于SDRE的变体飞行器LPV稳定控制

doi:10.12305/j.issn.1001-506X.2023.12.32

Abstract

Abstract:

Aiming at the problems of external disturbance and parameter uncertainty in the flight process of morphing aircraft, a linear parameter varying (LPV) stable flight control method based on state-dependent Riccati equation (SDRE) is proposed. Firstly, based on the aerodynamic parameter model and longitudinal nonlinear dynamic model of morphing aircraft, considering external disturbance, system parameter error and additional disturbance caused by deformation, the LPV system model is obtained by Jacobi linearization method. Then, for the LPV model considering composite interference, the control law based on SDRE is designed and solved by the θ-Dmethod. Finally, the Monte Carlo simulation verifies that the proposed method can effectively suppress the compound interference, realize the stable flight control of the aircraft, and has strong robustness and anti-interference ability.

Key words: morphing aircraft, state-dependent Riccati equation (SDRE), linear parameter varying (LPV), θ-D method, external disturbance, parameter uncertainty

CLC Number:

V249.1

Guangbin CAI, Dingkun MAO, Qian YANG, Xin LI, Mingzhe HOU. LPV stability control of morphing aircraft based on SDRE[J]. Systems Engineering and Electronics, 2023, 45(12): 4013-4020.

Figures/Tables 5

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Table 1

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References 31

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参数	符号/量纲	数值
质量	m/kg	1 247
转动惯量	I_y/(kg·m²)	4 067.5
气动弦长	c_A/m	1.74
参考面积	S_w/m²	17.09
最短翼展	b_min/m	10.18
最长翼展	b_max/m	20.36
推力	T/N	2 130
机翼翼型	-	NACA643.618

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LPV stability control of morphing aircraft based on SDRE

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References 31

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