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15篇 您的检索式:期刊名="Guidance Control Dyn"
    题名 作者 年代 出处 被引量
1Control System Optimization Using Genetic Algorithms显示文摘Krishnakumar K Goldberg D E 1994Guidance Control Dyn1994,,15:1
2Dynamics of a cantulaver beam attached to a moving base 显示文摘Kane T R Ryan R P Banerjee A K 1987J Guidance Control Dyn1987,10,2:1
3Sensor placements for on-orbit modal identification and correlation of large space structures显示文摘KAMMER D C 1991AIAA J of Guidance Control and Dyn1991,14,2:1
4Optimal sensor placement of large flexible space structures显示文摘TONGCO E MELDRUM D 1996AIAA J of Guidance Control and Dyn1996,19,4:1
5H ist orical review of airbearing spacecraft simul at ors显示文摘Jana L S Mas on A P Ch fist opher D H 2003Journ al of Guidance Control and Dyn ami cs2003,26,4:1
6Identification of Aerodynamic Coefficients Using Computational Neural Networks显示文摘LINSE D J STRENGEL R F 1993Guidance Control Dyn1993,16,6:1
7Survey of numerical methods for Trajectory optimiza- tion显示文摘BETTS J T 1998Guidance Control Dyn1998,21,2:1
8Disturbance attenuation and H∞ optimization with linear output feedback control显示文摘GU G MISRA P 1994J Guidance Control and Dyn1994,17,1:1
9Numerical approach for solving rigid spacecraft minimum time attitude maneuvers显示文摘Li F Bainum P M 1994Guidance Control Dyn1994,13,1:1
10Optimal continuous torque attitude ma-neuvers显示文摘Junkins J L Turner J D 1980Guidance Control Dyn1980,3,3:1
11Survey of time-optimal attitude maneuvers显示文摘Scrivener S L Thomson R C 1994Guidance Control Dyn1994,17,2:1
12New results on the optimal spacecraft attitude maneuver problem显示文摘Vadali S R Kraige L G Junkins J L 1984Guidance Control Dyn1984,7,3:1
13Optimal nonlinear feedback control for spacecraft attitude maneuvers显示文摘Carrington C K Junkins J L 1986Guidance Control Dyn1986,9,1:1
14New penalty functions and optimal control formulation for spacecraft attitude control problems显示文摘Schaub H Junkins J L 1997Guidance Control Dyn1997,20,3:1
15Exact nonlinear control of spacecraft slowing maneuvers with internal maneuver transfer显示文摘Dwyer T A W 1986Guidance Control Dyn1986,9,2:1
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