Paper information

Paper code

IAC-17,C1,4,4,x41530

Order

4

Room

Hall A

Title

Ascent Flight Control of Launch Vehicle Using Angle of Attack Estimator

abstract

View PDF

Session

4. Guidance, Navigation & Control (2)

symposium

C1. ASTRODYNAMICS SYMPOSIUM

congress

IAC-17

Type of presentation

oral

Main author

Mr. Ario Birmiawan Widyoutomo, The Graduate Universty for Advanced Studies (SOKENDAI), Japan

Co-authors

Prof. Yasuhiro Morita, Japan Aerospace Exploration Agency (JAXA), Japan;