2020
DOI: 10.1109/access.2020.3044589
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Aerodynamic Statistics-Based Trajectory Estimation of Hypersonic Maneuvering Target

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Cited by 10 publications
(8 citation statements)
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“…is based on the prevalent simplifications (Li et al, 2015) that (i) the Earth is a nonrotating uniform sphere, and (ii) the HGV's sideslip angle is negligible, leaving attitude and trajectory to be fully described by the angle of attack and bank angle. Furthermore, the commanded/desired acceleration is assumed to be zero (Hough, 2017;Cheng et al, 2020).…”
Section: Aerodynamics Modellingmentioning
confidence: 99%
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“…is based on the prevalent simplifications (Li et al, 2015) that (i) the Earth is a nonrotating uniform sphere, and (ii) the HGV's sideslip angle is negligible, leaving attitude and trajectory to be fully described by the angle of attack and bank angle. Furthermore, the commanded/desired acceleration is assumed to be zero (Hough, 2017;Cheng et al, 2020).…”
Section: Aerodynamics Modellingmentioning
confidence: 99%
“…However, the absence of flight test data serving as ground truth poses two difficulties: (i) parameter values cannot be estimated from data, (ii) models cannot be validated. Academic researchers have been coping with these difficulties through parametric modelling, where a geometric model (Cheng et al, 2020) or aerodynamic model (Liu et al, 2018b) or manoeuvre model (Hu et al, 2021) is parameterised and subjected to simulations for the determination of suitable parameter values. For example,…”
Section: Aerodynamics Modellingmentioning
confidence: 99%
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