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25篇 您的检索式:作者名="SAHJENDRA"
    题名 作者 年代 出处 被引量
1Output feedback adaptive variable structure control of chaos in Lorenz system显示文摘Aldayr D A Sahjendra N S 2002International Journal of Bifurcation and Chaos2002,12,3:2
2Nonlinear predictive control of feedback linearizable systems and flight control system design显示文摘Singh Sahjendra N Steinberg M Digirolamo R D 1995Journal of Guide Cont and Dynamias1995,18,5:1
3Adaptive optimal control of an au- tonomous underwater vehicle in the dive plane using dorsal fins 显示文摘MUKUND N SAHJENDRA N S 2006Ocean Engineering2006,33,3:1
4Simplified adaptive control of an orbiting flexible spacecraft显示文摘GANESH B M SAHJENDRA N S 0,,:1
5Direct adaptive and neural control of wing-rock motion of slender delta wings 显示文摘Sahjendra N Singh 1995Journal of Guidance Control and Dynamics (S0731-5090)1995,18,1:1
6Nonlinear decoupling sliding mode control and attitude control of spacecraft显示文摘Sahjendra N S Ashok I 1989IEEE Transactions on Aerospace and Electronic Systems1989,25,5:1
7Adaptive Con- trol and Stabilization of Elastic Spacecraft 显示文摘Sahjendra N Singh Aldayr D de Araujo AIAA- 97-3747 : 1526-15340,,:1
8Output Feedback Modular Adaptive Control of a Nonlinear Proto Typical Wing Section 显示文摘Nilesh B Sahjendra N S 2004Nonlinear Dynamics2004,37,4:1
9Adaptive Output Feed- back Control of Spacecraft with Flexible Appendages by Modeling Error Compensation 显示文摘Sahjendra N Singh Rong Zhang 2004Acta Astronautica2004,,54:1
10Adaptive Control of Spacecraft with Flexible Appendages Using Nussbaum Gain 显示文摘Keum W Lee Sahjendra N Singh 2007AIAA-2007-64332007,6433,:1
11Adaptive Control of Feedback Linearizable Nonlinear Systems with Application to Flight Control显示文摘 Marc Steinberg 1996Journal of Guidance Control and Dynamics1996,19,4:1
12Adaptive Control of Feedback Linearizable Nonlinear Systems with Application to Flight Control显示文摘Sahjendra N Singh Marc Steinberg 1996Journal of Guidance Control and Dynamics1996,19,4:1
13State-dependent Riccati equation-based robust dive plane control of AUV with control constraints显示文摘MUGDHA N SAHJENDRA N 0,,11:1
14Feedback linearization and solar pressure satellite attitude control显示文摘 Woosoon Y 1996IEEE Trans on Aerospace and Electronic Systems1996,32,2:1
15Nonlinear decoupling sliding mode control and attitude control of spacecraft显示文摘 Ashok I 1989IEEE Trans on Aerospace and Electronic Systems1989,25,5:1
16Simplified adaptive control of an orbiting flexible spacecraft显示文摘GANESH B M SAHJENDRA N S 2007Acta Astronautiea2007,61,4:1
17State feedback control of an aeroelastic system with structural nonlinearity 显示文摘Sahjendra N Singh Woosoon Yim 2003Aerospace Science and Technology2003,7,:1
18Feedback linearization and solar pressure satellite attitude control显示文摘SAHJENDRA N S WOOSOON Y 1996IEEE Trans on Aerospace and Electronic Systems1996,32,2:1
19Nonlinear decoupling sliding mode control and attitude control of spacecraft显示文摘SAHJENDRA N S ASHOK I 1989IEEE Trans on Aerospace and Electronic Systems1989,25,5:1
20Adaptive control of a nonlinear aeroelastic system despite gust load显示文摘Keum W Lee Sahjendra N Singh 2013Journal of Vibration and Control2013,19,12:1
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