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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Bibliographic Details
Main Authors: Luís M. B. C. Campos, Paulo J. S. Gil
Format: Artigo
Language:Inglês
Published: MDPI AG 2020-09-01
Series:Aerospace
Subjects:
rocket trajectories
analytical methods
variable mass
nonlinear aerodynamic forces
atmospheric stratification
Online Access:https://www.mdpi.com/2226-4310/7/9/131
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