Author: Peter Alexander BidianPublisher:
ISBN:
Category :
Languages : en
Pages : 310
Book Description
Piecewise Constant Guidance for Aeroassisted Orbit Transfer
Author: Peter Alexander BidianPublisher:
ISBN:
Category :
Languages : en
Pages : 310
Book Description
Piecewise-constant Control Strategies for Use in Minimum Fuel Aeroassisted Orbital Transfers
Author: Anthony Baker PagePublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 164
Book Description
Development and comparison of optimal guidance laws for aeroassisted orbit transfer
Author: Jalal MaparPublisher:
ISBN:
Category : Orbital transfer (Space flight)
Languages : en
Pages : 152
Book Description
Aeroassisted Orbital Transfer
Author: D.Subbaram NaiduPublisher: Springer
ISBN: 9783662182536
Category : Technology & Engineering
Languages : en
Pages : 182
Book Description
The concept of aeroassisting for orbital transfer has been recognized as one of the critical technologies for pioneering the space frontier. In space transportation systems, aeroassisting (or aerobraking), defined as the deceleration resulting from the effects of atmospheric drag upon a vehicle during orbital operations, opens new mission opportunities, especially with regard to the establishment of the permanent Space Station Freedom and space explorations to other planets such as Mars. The main areas of research reported in this monograph are atmospheric entry problem by the method of matched asymptotic expansions, coplanar and non-coplanar orbital transfers with aeroassist technology, orbital plan change with aerocruise, and neighbouring optimal guidance. A special feature is the bibliography which will provide the reader with a literature status for further research.
Nearly-optimal Highly-robust Guidance for Aeroassisted Orbital Transfer
Author: A. MieleScientific and Technical Aerospace Reports
Author: Robust Approximate Optimal Guidance Strategies for Aeroassisted Orbital Transfer Missions
Author: Marc R. IlgenNeighboring Optimal Guidance for Aeroassisted Orbital Transfer in the Presence of Modelling and Measurement Uncertainties
Author: C. CharalambousAeroassisted Orbital Transfer
Author: Desineni S. NaiduPublisher: Springer Verlag
ISBN: 9780387198194
Category : Technology & Engineering
Languages : en
Pages : 178
Book Description
The concept of aeroassisting for orbital transfer has been recognized as one of the critical technologies for pioneering the space frontier. In space transportation systems, aeroassisting (or aerobraking), defined as the deceleration resulting from the effects of atmospheric drag upon a vehicle during orbital operations, opens new mission opportunities, especially with regard to the establishment of the permanent Space Station Freedom and space explorations to other planets such as Mars. The main areas of research reported in this monograph are atmospheric entry problem by the method of matched asymptotic expansions, coplanar and non-coplanar orbital transfers with aeroassist technology, orbital plan change with aerocruise, and neighbouring optimal guidance. A special feature is the bibliography which will provide the reader with a literature status for further research.
Development of Closed-form Optimal Guidance Law for Aero-assisted Orbit Transfer
Author: Padmanabhan K. A. MenonPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages :
Book Description