Rocket Boost Trajectories for Maximum Burnout Velocity
Author:
Affiliation:
1. Convair-Fort Worth Div., General Dynamics Corp., Fort Worth, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.5171
Reference6 articles.
1. Trajectory programming for maximum range
2. The Optimization of Trajectories
Cited by 11 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Minimum-fuel thrust-limited transfer trajectories between coplanar elliptic orbits;AIAA Journal;1970-10
2. Optimal longitudinal control for obstacle clearance on takeoff;Guidance, Control and Flight Mechanics Conference;1970-08-16
3. Minimum-fuel thrust-limited transfer trajectories between coplanar elliptic orbits;Astrodynamics Conference;1969-08-16
4. Flugleistungen der drehsymmetrischen Flugkörper;Grundzüge der Flugmechanik und Ballistik;1969
5. A survey of dynamic analysis methods for airframe-flight control design;Control and Flight Dynamics Conference;1968-08-12
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