NDLI: Actuator Constrained Optimal Formation Keeping Near the Libration Points

Content Provider	Springer Nature Link
Author	Marchand, B. G. Stanton, S. A.
Copyright Year	2009
Abstract	Spacecraft formations that evolve near the libration points of the Sun—Earth/Moon system are one option commonly considered for space-based interferometry applications. Although precision tracking is often envisioned as a requirement, earlier studies have already revealed that the dynamically sensitive nature of this region of space presents a number of unique challenges in this respect. For instance, physical hardware limitations, specifically related to the on-board actuators, can limit the attainable tracking accuracy. The goal of this investigation is to devise a numerical process that allows the designer to identify the maximum tracking accuracy achievable in the presence of actuator (e.g., thruster) constraints. This is accomplished through the application of direct optimization methods. A problem formulation is presented that effectively treats, within a nonlinear programming framework, problems with state and control discontinuities and problems involving temporally continuous but spatially discrete control variables. The results of this investigation lay the algorithmic foundation for future explorations involving multiple independent actuators each with its own set of constraints and switching dependencies.
Starting Page	607
Ending Page	632
Page Count	26
File Format	PDF
ISSN	00219142
Journal	The Journal of the Astronautical Sciences
Volume Number	57
Issue Number	3
e-ISSN	21950571
Language	English
Publisher	Springer-Verlag
Publisher Date	2013-03-21
Publisher Place	New York
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Extraterrestrial Physics, Space Sciences Mathematical Applications in the Physical Sciences Aerospace Technology and Astronautics
Content Type	Text
Resource Type	Article
Subject	Aerospace Engineering Space and Planetary Science

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

Natural Regions Near the Collinear Libration Points Ideal for Space Observations with Large Formations

Control of Spacecraft Formations Around the Libration Points Using Electric Motors with One Bit of Resolution

On the R4BP when Third Primary is an Ellipsoid

Libration point stationkeeping using the θ-D technique

Optimal altitude-constrained low-thrust transfer between inclined Circular Orbits

A Study of Libration Points in Modified CR3BP Under Albedo Effect when Smaller Primary is an Ellipsoid

Optimal lunar swingby trajectories

Adaptive spacecraft attitude tracking control with actuator uncertainties

New Approaches for Human Deep-Space Exploration

Actuator Constrained Optimal Formation Keeping Near the Libration Points

Similar Documents

Natural Regions Near the Collinear Libration Points Ideal for Space Observations with Large Formations

Control of Spacecraft Formations Around the Libration Points Using Electric Motors with One Bit of Resolution

On the R4BP when Third Primary is an Ellipsoid

Libration point stationkeeping using the θ-D technique

Optimal altitude-constrained low-thrust transfer between inclined Circular Orbits

A Study of Libration Points in Modified CR3BP Under Albedo Effect when Smaller Primary is an Ellipsoid

Optimal lunar swingby trajectories

Adaptive spacecraft attitude tracking control with actuator uncertainties

New Approaches for Human Deep-Space Exploration

Actuator Constrained Optimal Formation Keeping Near the Libration Points