Optimal trajectories of air and space vehicles-Reference-Cited by-同舟云学术

Optimal trajectories of air and space vehicles

Published:2004-04 Issue:2 Volume:76 Page:193-214
ISSN:0002-2667
Container-title:Aircraft Engineering and Aerospace Technology
language:en
Short-container-title:Aircraft Eng & Aerospace Tech

Author:

Bolonkin Alexander

Publisher

Emerald

Reference6 articles.

1. Bolonkin, A.A. (1965), “Optimization of trajectory of multistage flight vehicles”,Researches of Flight Dynamics, Masinobilding, Moscow, pp. 20‐78 (in Russian).

2. Bolonkin, A.A. (1968), “Solution general linear optimal problem with one control”,Pricladnaya Mechanica, Vol. 4 No. 4, pp. 111‐22, Moscow (in Russian).

3. Bolonkin, A.A. and Khot, N.S. (1994a), “Method for finding a global minimum”,AIAA/NASA/USAF/SSMO Symposium on Multidisciplinary Analysis and Optimization, 7‐9 September, Panama City, FL, USA.

4. Optimal bounded control design for vibration suppression

5. Miele, A. (1958), “General variable theory of the flight paths of rocket‐powered aircraft, missile and satellite carries”,Astronautica Acta, Vol. 4, pp. 256‐88.

Cited by 10 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. An Intelligent Hybridization of ABC and LM Algorithms With Constraint Engineering Applications;Handbook of Neural Computation;2017

2. Electrostatic Climber for Space Elevator and Launcher;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

3. Electrostatic AB‐Ramjet space propulsion for interplanetary flight;Aircraft Engineering and Aerospace Technology;2007-01-30

4. Electrostatic linear engine;Aircraft Engineering and Aerospace Technology;2006-11-01

5. Electrostatic Solar Wind Propulsion System;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10