Approximate analytical method of calculating the trajectories of an aircraft in the atmosphere

DOI10.1016/0021-8928(83)90023-0zbMath0546.70026OpenAlexW2071279262MaRDI QIDQ798019

N. L. Sokolov, N. M. Ivanov, Alexandr I. Martynov

Publication date: 1984

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(83)90023-0

zbMATH Keywords

heat insulationhigh density atmospheremotion of an aircraftplanet rotation

Mathematics Subject Classification ID

Free motion of a rigid body (70E15) Orbital mechanics (70M20)

Cites Work

• Optimum maneuvers of a skip vehicle with bounded lift constraints
• On a method of successive approximations for the solution of problems of optimal control
• Matched asymptotic solutions for optimum lift controlled atmosphericentry

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