LAREDO: Extension of a RvD tool for Lissajous scenarios - ESA

More documents

Recommendations

Info

DESCRIPTIONLAREDO© GMV, 2006 Property of GMVAll rights reserved
LAREDO Description (1)! LAREDO optimizes the launch trajectory, given the desiredfinal orbit and the rocket performances.– It includes constraints in the aerothermal flux.– A two phases launcher is used, with a coast arc (the phases durationis one of the optimised variables).! LAREDO simulates a chaser manoeuvre sequence, in order toRvD with the target in circular, elliptical and Lissajous orbits.– The target is passive.– The chaser performs a sequence of predefined manoeuvres.LAREDO: Extension for Lissajous scenarios 2006/10/05 Page 7 © GMV, 2006
Page 1 and 2: 3 rd ESA Workshop on Astrodynamics
Page 3: INTRODUCTION© GMV, 2006 Property o
Page 8 and 9: LAREDO Description (2)! Circular ma
Page 10 and 11: LAREDO Description (4)! Attitude mo
Page 12 and 13: LAREDO Description (6)! The Toolinc
Page 14 and 15: LAREDO Description (8)! Figures ofM
Page 16 and 17: LAGRANGE POINTS DYNAMICS (1)! The L
Page 18 and 19: LAGRANGE POINTS DYNAMICS (3)! The d
Page 20 and 21: LAGRANGE POINTS DYNAMICS (5)! A Lis
Page 22: Computation ofRvD MANOEUVRES© GMV,
Page 26 and 27: LAREDOCONCLUSIONS© GMV, 2006 Prope
Page 28 and 29: LAREDOQUESTIONS© GMV, 2006 Propert

LAREDO: Extension of a RvD tool for Lissajous scenarios - ESA

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?