Comparison of real-time guidance options for discrete-event drag modulation entry at mars

Keyphrases

• Predictive Algorithm 100%
• Coefficient Ratio 100%
• Mars 100%
• Discrete Event 100%
• Entry Condition 100%
• Numerics 100%
• Real-time Guidance 100%
• Ballistic Coefficient 100%
• Drag Modulation 100%
• Monte Carlo Method 50%
• Single-stage 50%
• Flight Performance 50%
• Vehicle Parameters 50%
• Flight Path Angle 50%
• Guidance Algorithm 50%
• Three Degrees of Freedom 50%
• Condition Variables 50%
• Property Condition 50%
• Entry Vehicle 50%
• Numerical Predictor-corrector 50%
• Landing Accuracy 50%

Engineering

• Corrector 100%
• Initial Condition 33%
• Degree of Freedom 33%
• Flight Path Angle 33%