AEROSPACE SHANGHAI, Volume. 41, Issue 4, 1(2024)
Fixed Time Control of RLV landing Section Under the Influence of Complex Wind Field
[3] M YOU, Q ZONG, B TIAN et al. Nonsingular terminal sliding mode control for reusable launch vehicle with atmospheric disturbances. Proceedings of the Institution of Mechanical Engineers, 232, 2019-2033(2018).
[8] O SMITH, S ADELFANG. A compendium of wind statistics and models for the NASA space shuttle and other aerospace vehicle programs:1998-208859(1998).
[9] S MULGUND, R STENGEL. Optimal nonlinear estimation for aircraft flight control in wind shear. Automatica, 32, 3-13(1996).
[10] P BALDI, P CASTALDI, N MIMMO et al. A new longitudinal flight path control with adaptive wind shear estimation and compensation, 6852-6857(2011).
[11] J JUANG, K CHENG. Application of neural networks to disturbances encountered landing control. IEEE Transactions on Intelligent Transportation Systems, 7, 582-588(2006).
[12] Y DU, Q WU, C JIANG et al. Adaptive recurrent functional-link-network control for hypersonic vehicles with atmospheric disturbances. Science China Information Sciences, 54, 482-497(2011).
[13] G ZHANG, L YANG, J ZHANG et al. Longitudinal attitude controller design for aircraft landing with disturbance using ADRC/LQR, 330-335(2013).
[14] C HALL, Y SHTESSEL. Sliding Mode Disturbance Observer-Based Control for a Reusable Launch Vehicle. Journal of Guidance Control & Dynamics, 29, 1315-1328(2006).
[15] L ZHANG, X JU, N CUI. Ascent control of heavy-lift launch vehicle with guaranteed predefined performance. Aerospace Science and Technology, 110, 106511(2021).
[16] P TIAN, H CHAO, M RHUDY et al. Wind sensing and estimation using small fixed-wing unmanned aerial vehicles:A survey. Journal of Aerospace Information Systems, 18, 132-143(2021).
[18] S WASLANDER, C WANG. Wind disturbance estimation and rejection for quadrotor position control, 1-14(2009).
[21] L CAO, B XIAO, M GOLESTANI et al. Faster fixed-time control of flexible spacecraft attitude stabilization. IEEE Transactions on Industrial Informatics, 16, 1281-1290(2019).
[22] B TIAN, Q ZONG, J WANG et al. Quasi-continuous high-order sliding mode controller design for reusable launch vehicles in reentry phase. Aerospace science and technology, 28, 198-207(2013).
[24] A POLYAKOV. Nonlinear feedback design for fixed-time stabilization of linear control systems. IEEE Transactions on Automatic Control, 57, 2106-2110(2011).
[25] L CAO, B XIAO, M GOLESTANI et al. Faster fixed-time control of flexible spacecraft attitude stabilization. IEEE Transactions on Industrial Informatics, 16, 1281-1290(2019).
[26] Z ZUO. Nonsingular fixed-time consensus tracking for second-order multi-agent networks. Automatica, 54, 305-309(2015).
[27] M BASIN, P YU, Y SHTESSEL. Finite‐and fixed‐time differentiators utilising HOSM techniques. IET Control Theory & Applications, 11, 1144-1152(2017).
[28] C WEI, M WANG, B LU et al. Accelerated Landweber iteration based control allocation for fault tolerant control of reusable launch vehicle. Chinese Journal of Aeronautics, 35, 175-184(2022).
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Naigang CUI, Guoxin QU, Yuhao ZHANG. Fixed Time Control of RLV landing Section Under the Influence of Complex Wind Field[J]. AEROSPACE SHANGHAI, 2024, 41(4): 1
Category: Special Paper of Expert
Received: Jun. 25, 2024
Accepted: --
Published Online: Nov. 18, 2024
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