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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Bibliografische gegevens
Hoofdauteurs: Luís M. B. C. Campos, Paulo J. S. Gil
Formaat: Artigo
Taal:Inglês
Gepubliceerd in: MDPI AG 2020-09-01
Reeks:Aerospace
Onderwerpen:
rocket trajectories
analytical methods
variable mass
nonlinear aerodynamic forces
atmospheric stratification
Online toegang:https://www.mdpi.com/2226-4310/7/9/131
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