IEEE Congress on Evolutionary Computation, CEC 2015


Article Details
Title: Robust trajectory optimization of space launch vehicle using computational intelligence
Article URLs:
Alternative Article URLs: en.journals.sid.ir/ViewPaper.aspx?ID=465343
Authors: Ali A. Bataleblu
  • K.N. Toosi University of Technology Tehran, Iran, Department of Aerospace Engineering
Jafar Roshanian
  • K.N. Toosi University of Technology Tehran, Iran, Department of Aerospace Engineering
Sharing: Research produced no artifacts
Verification: Authors have verified information
Artifact Evaluation Badge: none
Artifact URLs:
Artifact Correspondence Email Addresses:
NSF Award Numbers:
DBLP Key: conf/cec/BatalebluR15
Author Comments: Despite the usefulness of Uncertainty-based Design Optimization (UDO), computational burden associated with uncertainty propagation and analysis process still remains as a major challenge of this field of study.

Discuss this paper and its artifacts below