Add to ORKGEffort was directed toward the problems of the real time trajectory optimization and guidance law development for the National Aerospace Plane (NASP) applications. In particular, singular perturbation methods were used to develop guidance algorithms suitable for onboard, real time implementation. The progress made in this research effort is reported
Data, tables, and graphs relative to the optimal trajectories for an aerospace plane are presented. ...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
Entry guidance equations, reference trajectories, and guidance system mechanizatio
The research on optimal trajectories for the National Aerospace Plane (NASP) performed by the Aero-A...
General problems associated with on-board trajectory optimization, propulsion system cycle selection...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
During the past six months the research objectives outlined in the last semi-annual report were acco...
Issued as Progress reports [nos. 1-3], and Final report, Project no. E-16-656Final report has title:...
A regular perturbation analysis is presented. Closed-loop simulations were performed with a first or...
The effort was in two areas: (1) development of advanced methods of flight path optimization, and (2...
A collection of analytical studies is presented related to unconstrained and constrained aircraft (a...
A real-time computer algorithm to control and optimize aircraft flight profiles is described and app...
A practical real time guidance algorithm has been developed for aerobraking vehicles that minimizes ...
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
This paper develops a near-optimal guidance law for generating minimum fuel, time, or cost fixed-ran...
Data, tables, and graphs relative to the optimal trajectories for an aerospace plane are presented. ...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
Entry guidance equations, reference trajectories, and guidance system mechanizatio
The research on optimal trajectories for the National Aerospace Plane (NASP) performed by the Aero-A...
General problems associated with on-board trajectory optimization, propulsion system cycle selection...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
During the past six months the research objectives outlined in the last semi-annual report were acco...
Issued as Progress reports [nos. 1-3], and Final report, Project no. E-16-656Final report has title:...
A regular perturbation analysis is presented. Closed-loop simulations were performed with a first or...
The effort was in two areas: (1) development of advanced methods of flight path optimization, and (2...
A collection of analytical studies is presented related to unconstrained and constrained aircraft (a...
A real-time computer algorithm to control and optimize aircraft flight profiles is described and app...
A practical real time guidance algorithm has been developed for aerobraking vehicles that minimizes ...
Three numerical procedures for Mayer classical and non-classical problems in trajectory optimizatio
This paper develops a near-optimal guidance law for generating minimum fuel, time, or cost fixed-ran...
Data, tables, and graphs relative to the optimal trajectories for an aerospace plane are presented. ...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
Entry guidance equations, reference trajectories, and guidance system mechanizatio