2001
DOI: 10.1029/2001ja000177
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Predicting the 1‐AU arrival times of coronal mass ejections

Abstract: Abstract.We describe an empirical model to predict the 1-AU •rrival of coronal mass ejections (CMEs). This model is based on an effective interplanetary (IP) acceleration described by Gopalswamy et al. [2000b] that the CMEs are subject to, as they propagate from the Sun to i AU. We have improved this model (1) by minimizing the projection effects (using data from spacecraft in quadrature) in determining the initial speed of CMEs, and (2) by allowing for the cessation of the interplanetary acceleration before … Show more

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Cited by 415 publications
(592 citation statements)
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“…Consequently, CMEs faster then solar wind decelerate, whereas slower ones are accelerated, both eventually being adjusted to the solar wind speed (e.g., Lindsay et al 1999, Gopalswamy et al 2001, Manoharan 2006, Vršnak &Žic 2007. In this paper the influence of the aerodynamic drag on the CME kinematics in the high corona and interplanetary space is analyzed, and implications for the space weather forecasting are discussed.…”
Section: Introductionmentioning
confidence: 99%
“…Consequently, CMEs faster then solar wind decelerate, whereas slower ones are accelerated, both eventually being adjusted to the solar wind speed (e.g., Lindsay et al 1999, Gopalswamy et al 2001, Manoharan 2006, Vršnak &Žic 2007. In this paper the influence of the aerodynamic drag on the CME kinematics in the high corona and interplanetary space is analyzed, and implications for the space weather forecasting are discussed.…”
Section: Introductionmentioning
confidence: 99%
“…The speed distributions for accelerating and decelerating events are nearly identical and to a worthy estimation they can be fitted with a single log-normal distribution [69]. However, to compute the acceleration is not an easy way because it depends on the projection effects and acceleration distance [70].…”
Section: Coronal Mass Ejections (Cmes)mentioning
confidence: 99%
“…We call R c a "deceleration cessation distance," which was originally discussed in the empirical models (Gopalswamy et al 2001). Solving Equation ( …”
Section: The Fundamental Condition For Extremely Fastmentioning
confidence: 99%
“…The ECA model assumes "effective" constant deceleration (or acceleration) of CMEs in interplanetary space. Gopalswamy et al (2001) introduced a deceleration cessation distance of 0.76 au, after which ICMEs propagate with a constant speed in order to improve the predictability of the ECA model. The empirical shock arrival model that Gopalswamy et al (2005) developed, and based on the combination of ECA model prediction and piston-driven shock propagation, predicts a 1 au arrival time for a leading shock front.…”
Section: Introductionmentioning
confidence: 99%