Paper information

Paper code

IAC-14,C1,8,5,x23635

Order

5

Room

801A

Title

Variable Specific Impulse Low-thrust Low Thrust Trajectory Optimization Using Homotopic Approach

abstract

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Session

8. Mission Design, Operations and Optimization (1)

symposium

C1. ASTRODYNAMICS SYMPOSIUM

congress

IAC-14

Type of presentation

oral

Main author

Mr. Junfeng Li, State Key Laboratory of Astronautic Dynamics (ADL), affiliated to Xi’an Satellite Control Center, Xi’an, China