Determination of guidance parameters of exo-atmospheric interceptors via miss distance error analysis

2001 ◽  
Author(s):  
David Pearson ◽  
Hari Hablani
2004 ◽  
Vol 27 (2) ◽  
pp. 283-289 ◽  
Author(s):  
Hari B. Hablani ◽  
David W. Pearson

1965 ◽  
Vol 21 ◽  
pp. 153-175
Author(s):  
D. O. Muhleman

This paper is devoted to an exact discussion of the determination of the astronomical unit with radar and to an extensive error analysis of the technique. Theoretical relationships between the constants are used to construct a consistent set of numerical values of constants based on these results.


2009 ◽  
Vol 14 (4-6) ◽  
pp. 69-82 ◽  
Author(s):  
J. Kozak ◽  
K. Krysztoforski ◽  
T. Kroll ◽  
S. Helbig ◽  
M. Helbig

Author(s):  
G. Satheesh Kumar ◽  
T. Nagarajan

Reconfiguration of Stewart platform for varying tasks accentuates the importance for determination of optimum geometry catering to the specified task. The authors in their earlier work (Satheesh et al., 2008) have indicated the non availability of an efficient holistic methodology for determining the optimum geometry. Further, they have proposed a solution using the variable geometry approach through the formulation of dimensionless parameters in combination with generic parameters like configuration and joint vector. The methodology proposed provides an approach to develop a complete set of design tool for any new reconfigurable Stewart platform for two identified applications viz., contour generation and vibration isolation. This paper details the experimental investigations carried out to validate the analytical results obtained on a developed Stewart platform test rig and error analysis is performed for contour generation. The experimental natural frequency of the developed Stewart platform has also been obtained.


Sign in / Sign up

Export Citation Format

Share Document