activity
20112018
most citedOptimal Thrust Level for Orbit Insertion

5 citations · 7 across the 10 of their papers we have counts for

collaborators

11 papers

math.OC2018

Coplanar Low-Thrust Transfer with Eclipses Using Analytical Costate Guess

Max Cerf

Low-thrust orbital transfers are difficult to optimize by indirect methods. The main issues come from the costate guess and from the numerical propagation accuracy required by the…

math.OC2018

Multiple Object Trajectography Using Particle Swarm Optimization Combined to Hungarian Method

Max Cerf

The problem of simultaneous trajectography of several dynamical objects is formulated as an optimization problem. The available observations consist in a series of photographs show…

math.OC2017

Why do launch trajectories end downwards

Max Cerf

The problem of finding the optimal thrust profile of a launcher upper stage is analyzed. The engine is assumed to be continuously thrusting, following either a linear or a bilevel…

math.OC2017

Geometric Optimal Control and Applications to Aerospace

Jiamin Zhu, Emmanuel Trélat, Max Cerf

This survey article deals with applications of optimal control to aerospace problems with a focus on modern geometric optimal control tools and numerical continuation techniques. G…

math.OC2016★ 5 cited

Optimal Thrust Level for Orbit Insertion

Max Cerf

The minimum-fuel orbital transfer is analyzed in the case of a launcher upper stage using a constantly thrusting engine. The thrust level is assumed to be constant and its value is…

math.OC2015★ 1 cited

Coupled attitude and trajectory optimization for a launcher tilting maneuver

Jiamin Zhu, Emmanuel Trélat, Max Cerf

We study the minimum time control problem of the launchers. The optimal trajectories of the problem may contain singular arcs, and thus chattering arcs. The motion of the launcher…