The effect of a meridional wind on a satellite orbit

In this paper theoretical formulae are derived which show the effect of a meridional (south to north) wind on a satellite orbit of eccentricity less than 0.2. The aerodynamic force acting on the satellite, which is normally important only over a small section of the orbit near perigee, is assumed to be in the direction opposite to the satellite’s motion relative to the ambient air, so that meridional motion of the upper atmosphere slightly alters the direction of the drag. The resulting changes in the satellite’s orbital inclination and the right ascension of the node are evaluated. For a satellite whose perigee remains near the equator, a consistent meridional wind of 100 m/s in the vicinity of perigee can change the orbital inclination by 0.02° as the orbital period decreases by 10 min ; but when perigee moves widely, the effect is generally much smaller.

For an earth satellite orbit of small eccentricity ( e < 0·2) formulae are derived for the changes per revolution produced by the atmosphere in the argument of perigee, in the right ascension of the ascending node, and in the orbital inclination. These changes are then expressed in terms of the change in length of the semi-major axis, and numerical values are obtained for satellite 1957 β . It is found that the rotation of the major axis in the orbital plane due to the atmosphere is significant, being most important for inclinations between 60 and 70°. The total rotation, due both to the gravitational potential and to the atmosphere, agrees reasonably well with the observed values. The oblateness of the atmosphere is found to have only a small effect on the changes in the orbital inclination and the right ascension of the ascending node.


The satellite Cosmos 482 (1972-23A) was launched on 31 March 1972 into an orbit of eccentricity 0.42 inclined at 52° to the equator, and decayed on 5 May 1981. Orbits have been determined daily in the last 15 days of its life from NORAD and U. S. Navy observations, with the aid of the R. A. E. orbit determination program PROP 6. The orbital accuracy was about 40 m radially and cross-track. Various properties of the upper atmosphere were determined by analysing four of the orbital elements. The decrease in orbital inclination gave two values for atmospheric rotation rate at heights near 200 km, a morning value of 0.90 ± 0.05 rev/day and an average value of 1.05 ± 0.10 rev/day. The variation in the right ascension of the node, after removal of perturbations due to gravity and atmospheric rotation, gave a value for the meridional wind at a similar height: the wind was weak, 20 ± 20 m/s north to south at 08 h local time. From the decrease in perigee distance, density scale heights were determined at heights of 180-220 km accurate to 3%, and were found to be significantly higher (by 6%) than those indicated by the COSPAR International Reference Atomsphere; at the high levels of solar activity prevailing in 1981, CIRA gives too low a scale height. Finally, the angular motion of perigee was analysed, and indicated a day-to-night variation in density 0.7 ± 0.1 of that given by CIRA , implying a value of 1.14 ± 0.02 for the ratio of maximum day-time to minimum night-time density at 180 km height in April-May 1981.


2018 ◽  
Vol 90 (1) ◽  
pp. 74-86
Author(s):  
Nai-ming Qi ◽  
Qilong Sun ◽  
Yong Yang

Purpose The purpose of this paper is to study the effect of J3 perturbation of the Earth’s oblateness on satellite orbit compared with J2 perturbation. Design/methodology/approach Based on the parametric variation method in the time domain, considering more accurate Earth potential function by considering J3-perturbation effect, the perturbation equations about satellite’s six orbital elements (including semi-major axis, orbit inclination, right ascension of the ascending node, true anomaly, eccentricity and argument of perigee) has been deduced theoretically. The disturbance effects of J2 and J3 perturbations on the satellite orbit with different orbit inclinations have been studied numerically. Findings With the inclination increasing, the maximum of the semi-major axis increases weakly. The difference of inclination disturbed by the J2 and J3 perturbation is relative to orbit inclinations. J3 perturbation has weak effect on the right ascension and argument of perigee. The critical angle of the right ascension and argument of perigee which decides the precession direction is 90° and 63.43°, respectively. The disturbance effects of J2 and J3 perturbations on the argument of perigee, right ascension and eccentricity are weakened when the eccentricity increases, simultaneously, the difference of J2 and J3 perturbations on argument of perigee, right ascension and argument of perigee decreases with eccentricity increasing, respectively. Practical implications In the future, satellites need to orbit the Earth much more precisely for a long period. The J3 perturbation effect and the weight compared to J2 perturbation in LEO can provide a theoretical reference for researchers who want to improve the control accuracy of satellite. On the other hand, the theoretical analysis and simulation results can help people to design the satellite orbit to avoid or diminish the disturbance effect of the Earth’s oblateness. Originality/value The J3 perturbation equations of satellite orbit elements are deduced theoretically by using parametric variation method in this paper. Additionally, the comparison studies of J2 perturbation and J3 perturbation of the Earth’s oblateness on the satellite orbit with different initial conditions are presented.


Meridional (south - to - north) winds in the upper atmosphere may be specified by the equivalent angular rotation rate, Ф and previous theories for the effect of meridional winds on satellite orbits have used Ф as the controlling parameter. In this report the theory is developed anew in terms of the parameter M = Ф Sec Ф, where Ф is the latitude. It is shown that in practice M is just as useful as Ф; and M has the advantage of leading to a much simpler and more accurate theory for expressing the changes in orbital inclination and right ascension of an orbit of any eccentricity (0 < e < 1) produced by meridional winds in an oblate atmosphere. The theory is developed in two parts: for high eccentricity ( e > 0.05) and for low eccentricity ( e < 0.05).


1968 ◽  
Vol 46 (10) ◽  
pp. S131-S135 ◽  
Author(s):  
B. K. Chatterjee ◽  
N. V. Gopalakrishnan ◽  
G. T. Murthy ◽  
S. Naranan ◽  
B. V. Sreekantan ◽  
...  

The following results on the low-energy (> 0.6 GeV and > 1.0 GeV) muons in air showers of size 105 to 2 × 107 at Ootacamund (800 g cm−2) are obtained: (1) The average total number of muons [Formula: see text] varies as Ne0.32 ± 0.2 for 105 < Ne < 106, and as Ne0.8 ± 0.15for 106 < Ne < 2 × 107. (2) In showers showing flat electron lateral structure, the [Formula: see text] variation with Ne is similar to (1). However, in steep showers, [Formula: see text] varies as Ne0.75 ± 0.15 in the whole size range 105 to 2 × 107. (3) "Muon-rich" showers of size < 106 have less energy in the electron–photon component compared to "normal" showers. No such difference is found for showers of size > 106. (4) There is a slight indication of a deficiency of muon-rich showers having a flat lateral distribution of electrons in the right ascension interval 15–21 hours for showers of size 106–107. A similar deficit of showers was observed by the Tokyo group for muon-rich showers in the same RA interval.


1823 ◽  
Vol 113 ◽  
pp. 39-52

The observations which have been made during the last summer, confirm in a very decided manner the results which formed the subject of my last communication; in which I laid before the Society the nature of the differences that exist between the computed places of the principal Stars of the Greenwich Catalogue, and those deduced from actual observation. It is not my present intention to offer any explana­tion of the cause of these phenomena, although many obvious conjectures present themselves, the value of which it will require perhaps many years to determine. It is now my principal object to consider the force of that explanation of the differences in question, which will most readily occur to every astronomer, namely, that the whole may arise either from error committed by the observer, or from defect in the instruments of observation: this objection being the more weighty from the circumstance, that the observations of three distant periods are employed, and that an error in those of either period (but particularly of the two latter) would ma­terially affect the result now under consideration. I believe that every person, in proportion to his experience in the use of astronomical instruments, (even of the most unexceptionable construction), will be cautious in admitting the accuracy of any results, with whatever care the observations may have been made, which appear to militate against any received theory of astronomy; and I shall have occasion myself to show, from the great discordances between instru­ments of the highest reputation, that this distrust is but too well founded. More particularly ought our suspicion to be excited, when such anomalies are found to exist, as bear some direct proportion to the zenith distances of the stars observed. In all such cases we should never hesitate, I think, to ascribe the anomalies to defective observation. If therefore in the present instance, any part of the discordances in question can be shown to depend on polar or zenith distances, I shall willingly admit, as to such part of them at least, that they are no otherwise of importance, than as affording data for leading to the detection of some hitherto undiscovered errors. The anomalies, however, that have led me on to this enquiry, and to which alone I attach any importance, are found to de­pend rather on the right ascensions, than on the declinations of the stars. Accordingly I found, while collecting observa­tions to form a catalogue for the present period, that I could more nearly predict the deviation of a star from its computed place, by knowing its right ascension, than its declination. Now it is not easy to conceive in what way the error of an instrument for measuring declination, fixed in the meridian, can be occasioned by any circumstance depending on the right ascension of a star to be observed.


1988 ◽  
Vol 36 (11) ◽  
pp. 1085-1093 ◽  
Author(s):  
D.G. King-Hele ◽  
Doreen M.C. Walker

1850 ◽  
Vol 1 ◽  
pp. 121
Author(s):  
Ernest Schubert
Keyword(s):  

1988 ◽  
Vol 133 ◽  
pp. 497-500
Author(s):  
Xu Tong-qi ◽  
Lu Pei-zhen ◽  
Chu Zong-yuan ◽  
Wang Shu-he

Optical positions of 16 radio stars have been derived from 40 cm astrograph at Zô-Sè. The reference catalogues are AGK3 and SAO, the average mean square error of single observation is 0″.058 in the right ascension and 0″.053 in declination. The magnitude difference has no significant effect on the observations.


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