کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
8132132 | 1523272 | 2018 | 29 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Effects of space weather on the ionosphere and LEO satellites' orbital trajectory in equatorial, low and middle latitude
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
علوم زمین و سیارات
علوم فضا و نجوم
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چکیده انگلیسی
We study the effects of space weather on the ionosphere and low Earth orbit (LEO) satellites' orbital trajectory in equatorial, low- and mid-latitude (EQL, LLT and MLT) regions during (and around) the notable storms of October/November, 2003. We briefly review space weather effects on the thermosphere and ionosphere to demonstrate that such effects are also latitude-dependent and well established. Following the review we simulate the trend in variation of satellite's orbital radius (r), mean height (h) and orbit decay rate (ODR) during 15 October-14 November 2003 in EQL, LLT and MLT. Nominal atmospheric drag on LEO satellite is usually enhanced by space weather or solar-induced variations in thermospheric temperature and density profile. To separate nominal orbit decay from solar-induced accelerated orbit decay, we compute r,h and ODR in three regimes viz. (i) excluding solar indices (or effect), where r=r0,h=h0 and ODR=ODR0 (ii) with mean value of solar indices for the interval, where r=rm,h=hm and ODR=ODRm and (iii) with actual daily values of solar indices for the interval (r,h and ODR). For a typical LEO satellite at hâ¯=â¯450â¯km, we show that the total decay in r during the period is about 4.20â¯km, 3.90â¯km and 3.20â¯km in EQL, LLT and MLT respectively; the respective nominal decay (r0) is 0.40â¯km, 0.34â¯km and 0.22â¯km, while solar-induced orbital decay (rm) is about 3.80â¯km, 3.55â¯km and 2.95â¯km. h also varied in like manner. The respective nominal ODR0 is about 13.5â¯m/day, 11.2â¯m/day and 7.2â¯m/day, while solar-induced ODRm is about 124.3â¯m/day, 116.9â¯m/day and 97.3â¯m/day. We also show that severe geomagnetic storms can increase ODR by up to 117% (from daily mean value). However, the extent of space weather effects on LEO Satellite's trajectory significantly depends on the ballistic co-efficient and orbit of the satellite, and phase of solar cycles, intensity and duration of driving (or influencing) solar event.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Advances in Space Research - Volume 61, Issue 7, 1 April 2018, Pages 1880-1889
Journal: Advances in Space Research - Volume 61, Issue 7, 1 April 2018, Pages 1880-1889
نویسندگان
Victor U.J. Nwankwo, Sandip K. Chakrabarti,