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1
RBF network based adaptive sliding mode control for solar sails
RBF network based adaptive sliding mode control for solar sails
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RBF network based adaptive sliding mode control for solar sails

Lian, Xiaobin ; Liu, Jiafu ; Wang, Chuang ; Yuan, Tiger ; Cui, Naigang

Aircraft engineering, 2018-11, Vol.90 (8), p.1180-1191 [Periódico revisado por pares]

Bradford: Emerald Publishing Limited

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2
Close approach analysis of space objects and estimation of satellite-debris collision probability
Close approach analysis of space objects and estimation of satellite-debris collision probability
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Close approach analysis of space objects and estimation of satellite-debris collision probability

Navabi, M ; Hamrah, R

Aircraft Engineering and Aerospace Technology, 2015-09, Vol.87 (5), p.483-492 [Periódico revisado por pares]

Bradford: Emerald Group Publishing Limited

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3
Dynamics of short tether-net system during deorbiting
Dynamics of short tether-net system during deorbiting
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Dynamics of short tether-net system during deorbiting

Liu, Jiafu ; Fan, Shen ; Siyuan, Rong ; Cui, Naigang

Aircraft Engineering and Aerospace Technology, 2015-05, Vol.87 (3), p.284-291 [Periódico revisado por pares]

Bradford: Emerald Group Publishing Limited

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4
Autonomous orbit and attitude determination of satellite using SEMOI
Autonomous orbit and attitude determination of satellite using SEMOI
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Autonomous orbit and attitude determination of satellite using SEMOI

Zhang, Y. ; Jing, W.X. ; Liu, L.K.

Aircraft Engineering and Aerospace Technology, 2008-01, Vol.80 (5), p.538-544 [Periódico revisado por pares]

Bradford: Emerald Group Publishing Limited

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5
Blending optimal algorithm for heliocentric solar sailing
Blending optimal algorithm for heliocentric solar sailing
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Blending optimal algorithm for heliocentric solar sailing

Shi, Xiaoning ; Guo, Jifeng ; Cui, Naigang ; Huang, Rong

Aircraft Engineering, 2013-01, Vol.85 (2), p.144-149 [Periódico revisado por pares]

Bradford: Emerald Group Publishing Limited

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6
A guidance algorithm for launch to equatorial orbit
A guidance algorithm for launch to equatorial orbit
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A guidance algorithm for launch to equatorial orbit

Marrdonny, Mahamadd ; Mobed, Mohammad

Aircraft Engineering, 2009-01, Vol.81 (2), p.137-148 [Periódico revisado por pares]

Bradford: Emerald Group Publishing Limited

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7
Optimal planetary rendezvous with an electric sail
Optimal planetary rendezvous with an electric sail
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Optimal planetary rendezvous with an electric sail

Huo, Mingying ; Mengali, Giovanni ; Quarta, Alessandro A

Aircraft Engineering and Aerospace Technology, 2016-07, Vol.88 (4), p.515-522 [Periódico revisado por pares]

Bradford: Emerald Group Publishing Limited

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8
On-line orbit planning and guidance for advanced upper stage
On-line orbit planning and guidance for advanced upper stage
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On-line orbit planning and guidance for advanced upper stage

Zhang, Liang ; Wei, Changzhu ; Diao, Yin ; Cui, Naigang

Aircraft engineering, 2019-05, Vol.91 (4), p.634-647 [Periódico revisado por pares]

Bradford: Emerald Publishing Limited

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9
Rotational and relative translational control for satellite electromagnetic formation flying in low earth orbit
Rotational and relative translational control for satellite electromagnetic formation flying in low earth orbit
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Rotational and relative translational control for satellite electromagnetic formation flying in low earth orbit

Fan, Li ; Hu, Min ; Yang, Mingqi

Aircraft engineering, 2017-10, Vol.89 (6), p.815-825 [Periódico revisado por pares]

Bradford: Emerald Publishing Limited

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10
Non-linear feedback optimal control law for minimum-time injection problem using fuzzy system
Non-linear feedback optimal control law for minimum-time injection problem using fuzzy system
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Non-linear feedback optimal control law for minimum-time injection problem using fuzzy system

Pourtakdoust, S.H. ; Rahbar, N. ; Novinzadeh, A.B.

Aircraft Engineering, 2005-01, Vol.77 (5), p.376-383 [Periódico revisado por pares]

Bradford: Emerald Group Publishing Limited

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