Optimal guidance for the space shuttle transition

Keyphrases

• Optimal Guidance 100%
• Guidance Function 50%
• Open-end 50%
• Guidance Method 50%
• Damping Length 50%
• Hypersonic Entry 50%
• Path Length Control 50%
• Unit Weight 50%
• Cross Range 50%
• Angle Modulation 50%
• Range Control 50%
• Fixed Terminal 50%
• Pilot Display 50%

Engineering

• Space Shuttle 100%
• Cross-Range 25%
• End Time 25%
• Open End 25%