Journals
Publish with us
Publishing partnerships
About us
Blog
International Journal of Aerospace Engineering
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
International Journal of Aerospace Engineering
/
2021
/
Article
/
Tab 1
/
Research Article
Multiconstrained Ascent Trajectory Optimization Using an Improved Particle Swarm Optimization Method
Table 1
The initial trajectory states.
Variable
Initial
Terminal
Units
Altitude
474
500
km
Velocity
6600
7669
m/s
Flight path angle
7.6
0.1
°