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                             16 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 A correlation study of satellite finite element model for coupled load analysis using transmissibility with modified correlation measures Lim, Jae Hyuk
2014
33 1 p. 82-91
10 p.
artikel
2 Controllability analysis and attitude path planning of underactuated spacecraft systems Zhang, Jiawei
2014
33 1 p. 76-81
6 p.
artikel
3 Design specifications of H2O2/kerosene bipropellant rocket system for space missions Moon, Yongjun
2014
33 1 p. 118-121
4 p.
artikel
4 Editorial Board 2014
33 1 p. IFC-
1 p.
artikel
5 Effect of low-temperature overload on fatigue crack growth retardation and prediction of post overload fatigue life Sahu, Vaneshwar Kr.
2014
33 1 p. 100-106
7 p.
artikel
6 Extended state observer based robust control of wing rock motion Kori, Deepak Kumar
2014
33 1 p. 107-117
11 p.
artikel
7 Fault diagnosis and fault tolerant control for nonlinear satellite attitude control systems Gao, Chunyan
2014
33 1 p. 9-15
7 p.
artikel
8 Foreign object damage on the leading edge of gas turbine blades Marandi, Seyed Masoud
2014
33 1 p. 65-75
11 p.
artikel
9 Improved neural-aided sliding mode controller for autolanding under actuator failures and severe winds Ismail, Shaik
2014
33 1 p. 55-64
10 p.
artikel
10 0–1 integer programming model for procedural separation of aircraft by ground holding in ATFM Ozgur, Metin
2014
33 1 p. 1-8
8 p.
artikel
11 Multi-objective multidisciplinary design of Space Launch System using Holistic Concurrent Design Mirshams, Mehran
2014
33 1 p. 40-54
15 p.
artikel
12 On satellite electrodynamic attitude stabilization Antipov, K.A.
2014
33 1 p. 92-99
8 p.
artikel
13 Sensitivity analysis of damping performances for passive shunted piezoelectrics Park, Jae-Won
2014
33 1 p. 16-25
10 p.
artikel
14 Space station overall mission planning using decomposition approach Lin, Kun-Peng
2014
33 1 p. 26-39
14 p.
artikel
15 Spherical and oblate Earth conical shadow models for LEO satellites: Applications and comparisons with real time data and STK to IRS satellites Srivastava, Vineet K.
2014
33 1 p. 135-144
10 p.
artikel
16 Strapdown stellar-inertial guidance system for launch vehicle Zhang, Lijun
2014
33 1 p. 122-134
13 p.
artikel
                             16 gevonden resultaten
 
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