Neighboring Optimal Guidance for Aeroassisted Orbital Plane Change

Neighboring Optimal Guidance for Aeroassisted Orbital Plane Change PDF Author: Jeng-Shing Chern
Publisher:
ISBN:
Category :
Languages : en
Pages : 11

Book Description


An optimal guidance law for the aeroassisted orbital plane change maneuver

An optimal guidance law for the aeroassisted orbital plane change maneuver PDF Author: James Matthew Giltner
Publisher:
ISBN:
Category : Orbital transfer (Space flight)
Languages : en
Pages : 260

Book Description


Neighboring Optimal Guidance for Aeroassisted Orbital Transfer in the Presence of Modelling and Measurement Uncertainties

Neighboring Optimal Guidance for Aeroassisted Orbital Transfer in the Presence of Modelling and Measurement Uncertainties PDF Author: C. Charalambous
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


Piecewise Constant Guidance for Aeroassisted Orbit Transfer

Piecewise Constant Guidance for Aeroassisted Orbit Transfer PDF Author: Peter Alexander Bidian
Publisher:
ISBN:
Category :
Languages : en
Pages : 310

Book Description


IAF90-303 - IAF90-349

IAF90-303 - IAF90-349 PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 358

Book Description


Optimal Aeroassisted Orbital Plane Change with Heating Rate Constraint

Optimal Aeroassisted Orbital Plane Change with Heating Rate Constraint PDF Author: Fu-Kuo Hsu
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


Fuel-Optimal Trajectories of Aeroassisted Orbital Transfer with Plane Change

Fuel-Optimal Trajectories of Aeroassisted Orbital Transfer with Plane Change PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722410049
Category :
Languages : en
Pages : 64

Book Description
The problem of minimization of fuel consumption during the atmospheric portion of an aeroassisted, orbital transfer with plane change is addressed. The complete mission has required three characteristic velocities, a deorbit impulse at high earth orbit (HEO), a boost impulse at the atmospheric exit, and a reorbit impulse at low earth orbit (LEO). A performance index has been formulated as the sum of these three impulses. Application of optimal control principles has led to a nonlinear, two-point, boundary value problem which was solved by using a multiple shooting algorithm. The strategy for the atmospheric portion of the minimum-fuel transfer is to start initially with the maximum positive lift in order to recover from the downward plunge, and then to fly with a gradually decreasing lift such that the vehicle skips out of the atmosphere with a flight path angle near zero degrees. Naidu, Desineni Subbaramaiah and Hibey, Joseph L. Unspecified Center...

Fuel-optimal Trajectories of Aeroassisted Orbital Transfer with Plane Change

Fuel-optimal Trajectories of Aeroassisted Orbital Transfer with Plane Change PDF Author: Desineni S. Naidu
Publisher:
ISBN:
Category : Orbital transfer (Space flight)
Languages : en
Pages : 120

Book Description


Spaceflight Mechanics 1993

Spaceflight Mechanics 1993 PDF Author: Robert G. Melton
Publisher:
ISBN:
Category : Celestial mechanics
Languages : en
Pages : 752

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 304

Book Description