Mathematical Problems in Engineering / 2016 / Article / Tab 1

Research Article

The Multiobjective Trajectory Optimization for Hypersonic Glide Vehicle Based on Normal Boundary Intersection Method

Table 1

Important node in Pareto front of multiobjective optimization solution.

Pareto frontMinimum peak heat solutionMaximum terminal range solution

Range (km)55976102
(W/cm2)67.92128.3

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