Abstract this chapter expands our development of an autonomous descent guidance algorithm which is able to deal with both the aerodynamic descent and the powered landing phases of a reusable rocketN the method uses sequential convex optimization applied to a cartesian representation of the equations of motionL and the transcription is based on the use of hp pseudospectral methodsN the major contributions of the formulation are a more systematic exploitation and separation of convex and nonM convex contributions to minimize the computation of the latterL the inclusion of highly nonlinear terms represented by aerodynamic accelerationsL a complete reformulation\ud of the problem based on the use of euler angle rates as control meansL an impro...
The field of aerospace guidance and control has recently been evolving from focusing on traditional ...
A novel algorithm for autonomous landing guidance computation is presented. The trajectory is expres...
AIAA Guidance, Navigation, and Control Conference and Exhibit AIAA 2003-5639 11-14 August 2003, Aust...
Abstract this chapter expands our development of an autonomous descent guidance algorithm which is a...
One part of spaceflight technology that has always been in demand is to go to space using a vehicle ...
In this paper a new drag-energy scheme, based on the use of pseudospectral methods and convex optim...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.In...
In this paper a new drag-energy scheme, based on the use of pseudospectral methods and convex optimi...
Of the many direct numerical methods, the pseudospectral method serves as an effective tool to solve...
Thesis (Ph.D.)--University of Washington, 2020The objective of this dissertation is to develop new t...
It is well-known that onboard, real-time, optimal trajectory generation for reusable launch vehicles...
In the frame of technology development for reusable launch vehicles and future planetary landing mis...
In this paper, we present enhancements on the powered descent guidance algorithm developed for Mars ...
which permits unrestricted use, distribution, and reproduction in any medium, provided the original ...
A novel sequential convex (SCvx) optimization scheme via the Chebyshev pseudospectral method is prop...
The field of aerospace guidance and control has recently been evolving from focusing on traditional ...
A novel algorithm for autonomous landing guidance computation is presented. The trajectory is expres...
AIAA Guidance, Navigation, and Control Conference and Exhibit AIAA 2003-5639 11-14 August 2003, Aust...
Abstract this chapter expands our development of an autonomous descent guidance algorithm which is a...
One part of spaceflight technology that has always been in demand is to go to space using a vehicle ...
In this paper a new drag-energy scheme, based on the use of pseudospectral methods and convex optim...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.In...
In this paper a new drag-energy scheme, based on the use of pseudospectral methods and convex optimi...
Of the many direct numerical methods, the pseudospectral method serves as an effective tool to solve...
Thesis (Ph.D.)--University of Washington, 2020The objective of this dissertation is to develop new t...
It is well-known that onboard, real-time, optimal trajectory generation for reusable launch vehicles...
In the frame of technology development for reusable launch vehicles and future planetary landing mis...
In this paper, we present enhancements on the powered descent guidance algorithm developed for Mars ...
which permits unrestricted use, distribution, and reproduction in any medium, provided the original ...
A novel sequential convex (SCvx) optimization scheme via the Chebyshev pseudospectral method is prop...
The field of aerospace guidance and control has recently been evolving from focusing on traditional ...
A novel algorithm for autonomous landing guidance computation is presented. The trajectory is expres...
AIAA Guidance, Navigation, and Control Conference and Exhibit AIAA 2003-5639 11-14 August 2003, Aust...