A trim problem formulation for maximum control authority using the Attainable Moment Set geometry

Engineering

• Problem Formulation 100%
• Control Force 80%
• Decision Variable 40%
• Deflection 40%
• Obtains 20%
• Equality Constraint 20%
• Aircraft Control 20%
• Angle-of-Attack 20%
• Pitch Control 20%
• Constrained Optimization Problem 20%
• Inequality Constraint 20%
• Wings 20%
• Total Drag 20%

INIS

• control 100%
• geometry 100%
• surfaces 27%
• lifts 16%
• applications 11%
• pitches 11%
• aircraft 11%
• distance 5%
• allocations 5%
• optimization 5%
• linear programming 5%
• elevation 5%
• configuration 5%
• drag 5%
• algorithms 5%
• constraints 5%