Analysis of solar radiation pressure induced coupled liberations of a gravity stabilized axisymmetric satellite

1979 ◽  
Vol 20 (3) ◽  
pp. 297-313 ◽  
Author(s):  
S. K. Shrivastava ◽  
Hari B. Hablani
Author(s):  
Rikushi KATO ◽  
Masanori MATSUSHITA ◽  
Hideyuki TAKAHASHI ◽  
Osamu MORI ◽  
Nobukatsu OKUIZUMI ◽  
...  

Science ◽  
1960 ◽  
Vol 131 (3404) ◽  
pp. 920-921 ◽  
Author(s):  
R. W. Parkinson ◽  
H. M. Jones ◽  
I. I. Shapiro

GPS Solutions ◽  
1999 ◽  
Vol 2 (3) ◽  
pp. 50-62 ◽  
Author(s):  
T. A. Springer ◽  
G. Beutler ◽  
M. Rothacher

2017 ◽  
Vol 60 (10) ◽  
pp. 2146-2154 ◽  
Author(s):  
K. Rajaiah ◽  
K. Manamohan ◽  
S. Nirmala ◽  
S.C. Ratnakara

2014 ◽  
Vol 51 (1) ◽  
pp. 381-384 ◽  
Author(s):  
Tomohiro Yamaguchi ◽  
Yuya Mimasu ◽  
Yuichi Tsuda ◽  
Makoto Yoshikawa

2021 ◽  
Vol 57 (2) ◽  
pp. 279-295
Author(s):  
L. O. Marchi ◽  
D. M. Sanchez ◽  
F. C. F. Venditti ◽  
A. F. B. A. Prado ◽  
A. K. Misra

In this work, we study the effects of solar radiation pressure (SRP) on the problem of changing the orbit of an asteroid to support planetary defense, scientific research, or exploitation of materials. This alternative considers a tethered reflective balloon (or a set of reflective balloons) attached to the asteroid, with a high area-to-mass ratio, to use the SRP to deflect a potentially hazardous asteroid (PHA) or to approximate the target asteroid to Earth. The tether is assumed to be inextensible and massless, and the motion is described only in the orbital plane of the asteroid around the Sun. The model is then used to study the effects that the tether length, the reflectivity coefficient, and the area-to-mass ratio have on the deviation of the trajectory of the asteroid.


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