Reachable-Orbit-Domain for Launch Vehicles Based on Polyhedron Approximation Method.
Zeming HaoHaifeng HuYong HeHuifeng LiPublished in: ASCC (2022)
Keyphrases
- computational cost
- synthetic data
- pairwise
- high precision
- dynamic programming
- closed form
- probabilistic model
- detection method
- similarity measure
- significant improvement
- high accuracy
- theoretical analysis
- life cycle
- real time
- segmentation method
- clustering method
- support vector machine svm
- computationally efficient
- model selection
- experimental evaluation
- computational complexity