Extremal rocket motion with maximum thrust in a linear central field

Journal of Spacecraft and Rockets

Volumn 38, Issue 5, 2001, Pages 765-776

  Azimov, Dilmurat M ^a,b   Bishop, Robert H ^a,c  

^a UNIVERSITY OF TEXAS AT AUSTIN   (United States)

^b NATIONAL UNIVERSITY OF UZBEKISTAN   (Uzbekistan)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; MANEUVERABILITY; MATHEMATICAL MODELS; ORBITAL TRANSFER; ORBITS; TRAJECTORIES; VECTORS; VELOCITY;

LINEAR CENTRAL FIELDS; NEWTONIAN FIELDS;

ROCKETS;

EID: 0035439084     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3744     Document Type: Article

References (9)

1. Analytical solutions for intermediate thrust arcs of rocket trajectories in a newtonian field
2. On an analytical solution of the optimum trajectory problem in a gravitation field
3. Optimal analytic multiburn trajectories
4. Analytic solution for constant thrust optimal-coast, minimum-propellant space trajectories
5. An introduction to the mathematics and methods of astro-dynamics