Pages that link to "Item:Q642298"

The following pages link to Optimal low-thrust trajectories to asteroids through an algorithm based on differential dynamic programming (Q642298):

Displaying 9 items.

• A continuous implementation of a second-variation optimal control method for space trajectory problems (Q378272) (← links)
• Global 4-D trajectory optimization for spacecraft (Q617231) (← links)
• Target selection and transfer trajectories design for exploring asteroid mission (Q987360) (← links)
• On the deflection of asteroids with mirrors (Q990364) (← links)
• Constructing Pontryagin extremals for the optimal control problem of asteroid fly-by (Q1040516) (← links)
• A hybrid differential dynamic programming algorithm for constrained optimal control problems. I: Theory (Q1937080) (← links)
• A hybrid differential dynamic programming algorithm for constrained optimal control problems. II: Application (Q1937082) (← links)
• Design of optimal spacecraft‐asteroid formations through a hybrid global optimization approach (Q3526266) (← links)
• The solution of some difficult problems in low-thrust interplanetary trajectory optimization (Q3815978) (← links)