Zobrazeno 1 - 9
of 9
pro vyhledávání: '"P. M. Bainum"'
Autor:
P A Capó-Lugo, P M Bainum
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 223:1125-1139
The hierarchical control scheme is used to obtain the solutions of two-point boundary value problems to correct the separation distance drifts of a pair of satellites within a constellation in highly elliptical orbits according to mission constraints
Autor:
P A Capó-Lugo, P M Bainum
Aimed at students, faculty and professionals in the aerospace field, this book provides practical information on the development, analysis, and control of a single and/or multiple spacecraft in space. This book is divided into two major sections: sin
Autor:
P. M. Bainum, Z. Li
Publikováno v:
Journal of Sound and Vibration. 177:539-553
This investigation is to apply the so-called momentum exchange feedback control concept and distributed piezoelectric actuator technology to the vibration control of a flexible spacecraft. The flexible model to be investigated is a rigid hub with a c
Autor:
P. M. Bainum, V. K. Kumar
Publikováno v:
Journal of Guidance and Control. 3:90-92
The equations of motion of an arbitrary flexible body in orbit are derived. The model includes the effects of gravity with all its higher harmonics. As a specific example, the motion of a long, slender, uniform beam in circular orbit is modeled. The
Autor:
P. M. Bainum, A. S. S. R. Reddy
The dynamics of orbiting shallow flexible spherical shell structures under the influence of control actuators was studied. Control laws are developed to provide both attitude and shape control of the structure. The elastic modal frequencies for the f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::242e7b6552e658d0a8a48ff431795af2
https://doi.org/10.1016/b978-0-08-029328-8.50046-3
https://doi.org/10.1016/b978-0-08-029328-8.50046-3
Autor:
K. S. Evans, P. M. Bainum
Publikováno v:
13th Aerospace Sciences Meeting.
Autor:
P. M. Bainum, K. S. Evans
Publikováno v:
Mechanics and Control of Flight Conference.
The three dimensional equations of motion for a cable connected space station - counterweight system are developed using a Lagrangian formulation. The system model employed allows for cable and end body damping and restoring effects. The equations ar
Autor:
V. K. Kumar, P. M. Bainum
Publikováno v:
19th Aerospace Sciences Meeting.
A mathematical model for the motion of a large, flexible shallow spherical shell in a circular orbit is presented. For small elastic displacements and attitude angles the linearized equations for the roll and yaw (out-of-plane) motions completely sep
Autor:
P. M. Bainum, S. Sen
Publikováno v:
11th Aerospace Sciences Meeting.
The stability of a dual-spin satellite system during the momentum wheel spin-up maneuver is treated both analytically and numerically. The dual-spin system consists of: a slowly rotating or despun main-body; a momentum wheel (or rotor) which is accel