To enable autonomous operations in future Reusable Launch Vehicles (RLVs), reconfigurable control and adaptive guidance will often be required to facilitate recovery of the mission following a major anomalous event such as an effector failure. An adaptive guidance system that works in conjunction with a reconfigurable controller and an autonomous trajectory command reshaping algorithm is presented. The guidance law utilizes a backstepping architecture to generate pitch rate commands that drive the inner-loop control system. Under extreme failure conditions the control surfaces can saturate in an attempt to meet commanded moments. In these cases, the guidance feedback gains are reduced to preserve stability margins in the guidance loops. A c...
This thesis considers the problem of generating optimal entry trajectories for a reusable launch veh...
Reprinted with permission of the American Institute of Aeronautics and Astronautics, Inc. See http:/...
Future launch vehicle concepts and technologies for expendable and reusable launch vehicles are curr...
A guidance system with reconfiguration capabilities has been developed for reusable launch vehicles ...
Abstract — This paper presents an adaptive guidance system approach applied to hypersonic Reusable L...
Published in Journal of Guidance Control and Dynamics, Vol. 29, No. 3, May–June 2006.Received 23 No...
There are a number of approaches to advanced guidance and control (AG&C) that have the potential for...
This thesis presents a guidance scheme for the Terminal Area Energy Management (TAEM) and Approach a...
Reconfigurable inner-loop control laws improve the fault tolerance of a vehicle to control effector ...
The next generation of reusable launch vehicles (RLVs) require significant improvements in guidance...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999.In...
Future launch vehicle concepts and technologies for expendable and reusable launch vehicles are curr...
A terminal area energy management (TAEM) guidance system for an unpowered reusable launch vehicle (R...
Bibliography: leaves 220-229.xxiv, 229 leaves : ill. (some col.) ; 30 cm.Investigates alternative re...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, Februar...
This thesis considers the problem of generating optimal entry trajectories for a reusable launch veh...
Reprinted with permission of the American Institute of Aeronautics and Astronautics, Inc. See http:/...
Future launch vehicle concepts and technologies for expendable and reusable launch vehicles are curr...
A guidance system with reconfiguration capabilities has been developed for reusable launch vehicles ...
Abstract — This paper presents an adaptive guidance system approach applied to hypersonic Reusable L...
Published in Journal of Guidance Control and Dynamics, Vol. 29, No. 3, May–June 2006.Received 23 No...
There are a number of approaches to advanced guidance and control (AG&C) that have the potential for...
This thesis presents a guidance scheme for the Terminal Area Energy Management (TAEM) and Approach a...
Reconfigurable inner-loop control laws improve the fault tolerance of a vehicle to control effector ...
The next generation of reusable launch vehicles (RLVs) require significant improvements in guidance...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999.In...
Future launch vehicle concepts and technologies for expendable and reusable launch vehicles are curr...
A terminal area energy management (TAEM) guidance system for an unpowered reusable launch vehicle (R...
Bibliography: leaves 220-229.xxiv, 229 leaves : ill. (some col.) ; 30 cm.Investigates alternative re...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, Februar...
This thesis considers the problem of generating optimal entry trajectories for a reusable launch veh...
Reprinted with permission of the American Institute of Aeronautics and Astronautics, Inc. See http:/...
Future launch vehicle concepts and technologies for expendable and reusable launch vehicles are curr...