MPC Trajectory Optimization

Receding Horizon Control with Constraint Handling for Fuel-Optimal Maneuvers

Prediction Horizon (N)20

Control Horizon (M)10

State Weight (Q)10

Control Weight (R)1

Optimization Results

Total ΔV--

Track Error RMS--

Solve Time--

Max Thrust (N)10

Max Rate (deg/s)5

Keep-out Zone (m)50

Constraint Status

Thrust Violations0

Rate Violations0

FeasibleYes

Analyze how prediction horizon affects performance and computation.

Recommendations

Optimal N--

Min Cost--