Flight Dynamics 2012 Issue 3 Design of nonlinear H∞ guidance law considered the effect of SNR

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Flight Dynamics
1002-0853
2012 Issue 3

Design of nonlinear H∞ guidance law considered the effect of SNR
WANG Guo-qing;GUO Jian-guo;ZHOU Jun

..............page:254-257,262

Establishment and validation on dynamics simulation model of separation of eccentric sub-satellite
SHEN Xiao-feng;XIAO Yu-zhi;KANG Zhi-yu

..............page:258-262

Study on the non-Keplerian orbits of the near space hypersonic vehicles
LI Hai-lin;WU De-wei

..............page:276-279

Development and key technologies of the waverider aerodynamic design optimization
GAN Wen-biao;ZHOU Zhou;ZHU Xiao-ping

..............page:193-196

fei xing li xue zheng gao jian ze

..............page:封4

Optimization of FCS parameter based on Pareto optimal set and multi-objective decision
XU Ning;DONG Xin-min;LIU Zong-cheng;CHEN Yong

..............page:245-249

Receding optimization method for on-line path planning in dynamic environment
WEI Tie-tao;WANG Jian-wei;QU Xiang-ju

..............page:218-222

Research on parameter-dependent robust controller for unmanned aircraft
ZHI Yue;ZHAO Guo-rong;SONG Chao

..............page:238-241

Design of instantaneous circular acceleration guidance law
LI Wei;WANG Zhi-gang;JIANG Qi-ying

..............page:272-275

Research on the feedforward structural DASA suppresser to prevent PIO
LI Ying-hui;ZHU Guang-dong;CAO Qi-meng;XU Hao-jun;MENG Jie

..............page:213-217,237

Integrated optimum design for ramjet missile climb trajectory and thrust regulation
SHANG Teng;GU Liang-xian;ZHAO Ji-song;GONG Chun-lin

..............page:280-283,288

Research on flight dynamics model of ducted fan MAV
CAI Hong-ming;ANG Hai-song;DENG Shuang-hou;ZHANG Hua-liang

..............page:197-200

Improved design and analysis on aerodynamics for a propeller-driven long-endurance UAV
LIU Cheng-bin;LI Jie;LI Xin;ZHOU Li-qiong

..............page:209-212

Research on a new combined guidance law for modern fighter
YANG Nan;ZHANG Jian;TANG Hua;OU Fei

..............page:228-232

Optimization of pitching angle during a pilotless aircraft rocket ejecting takeoff
RAN Hai-xia

..............page:242-244

Aeroservoelastic analysis of elastic aircraft
WANG Zheng;ZHAO Yu-shan;SHI Peng;LI Wen-long

..............page:233-237

Application of maximum likelihood estimation to the parameter identification of airplane take-off performance
YU Xue-mei;CHENG Wei;GU Wei-yan

..............page:201-205

Approach power compensator system for carrier-based aircraft with variable structure control
ZHU Qi-dan;LI Xin-fei;LV Kai-dong

..............page:223-227

Analysis of the control-oriented conceptual design optimization methods for hypersonic aerospace vehicles
SU Er-long;LUO Jian-jun;YAN Ying-xin;FANG Qun;HUANG Xing-li

..............page:267-271

Rapid approach for three-dimensional trajectory optimization of hypersonic reentry vehicles
LIU Peng;ZHAO Ji-song;GU Liang-xian

..............page:263-266,271

Concept study of lower surface spoiler for longitudinal control of the tailless configuration
SUN Jing;ZHANG Bin-qian;YANG Guang-jun

..............page:206-208

Entry trajectory optimization for suborbital launch vehicle based on mission safety
WANG Wen-hu;LI Xin-guo

..............page:284-288

Aerodynamic analysis on separation of cluster munition in near space
WANG Hong-wei;GUO Jian-guo;LIN Peng;ZHOU Jun

..............page:250-253