Practical optimization of low-thrust minimum-time orbital rendezvous in sun-synchronous orbits

Engineering

• Costate Variable 100%
• Rendezvous Problem 100%
• Orbital Element 50%
• Optimization Method 50%
• Numerical Example 50%
• Specific Impulse 50%
• Optimal Control 50%
• Optimal Control Problem 50%
• Averaging Technique 50%
• Optimisation Procedure 50%
• Electric Propulsion 50%
• Debris Removal 50%
• Oblateness 50%
• Pontryagins Maximum Principle 50%
• Osculating Element 50%
• Space Robotics 50%