The Two-Point Boundary-Value Problem for Rocket Trajectories

The two dimensional gravity turn problem is addressed allowing for the effects of variable rocket mass due to propellant consumption, thrust and thrust vector angle, lift and drag forces at an angle-of-attack and atmospheric mass density varying with altitude; Coriolis and centrifugal forces are neg...

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Detaylı Bibliyografya
Asıl Yazarlar: Luís M. B. C. Campos, Paulo J. S. Gil
Materyal Türü: Artigo
Dil:Inglês
Baskı/Yayın Bilgisi: MDPI AG 2020-09-01
Seri Bilgileri:Aerospace
Konular:
rocket trajectories
analytical methods
variable mass
nonlinear aerodynamic forces
atmospheric stratification
Online Erişim:https://www.mdpi.com/2226-4310/7/9/131
Etiketler: Etiketle
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