Interplanetary missions which use low-thrust, high specific impulse propulsion can further capitalise on the capabilities of the propulsion system by using it to effect escape from the launch body or capture at a target body.
Simple control laws for continuous-thrust escape or capture and their use in optimisation
AIAA/AAS Astrodynamics Conference
2002-08-05
Conference paper
No indication
English
British Library Conference Proceedings | 2002
|Simple control laws for low-thrust orbit transfers
NTRS | 2003
|