Published May 7, 2009 | Version v1
Journal article

Engineering of the LISA Pathfinder mission-making the experiment a practical reality

  • 1. EADS Astrium, Gunnels Wood Road, Stevenage, SG1 2AS (United Kingdom)

Description

LISA Pathfinder represents a unique challenge in the development of scientific spacecraft-not only is the LISA Test Package (LTP) payload a complex integrated development, placing stringent requirements on its developers and the spacecraft, but the payload also acts as the core sensor and actuator for the spacecraft, making the tasks of control design, software development and system verification unusually difficult. The micro-propulsion system which provides the remaining actuation also presents substantial development and verification challenges. As the mission approaches the system critical design review, flight hardware is completing verification and the process of verification using software and hardware simulators and test benches is underway. Preparation for operations has started, but critical milestones for LTP and field effect electric propulsion (FEEP) lie ahead. This paper summarizes the status of the present development and outlines the key challenges that must be overcome on the way to launch.

Availability note (English)

Available from http://dx.doi.org/10.1088/0264-9381/26/9/094002

Additional details

Identifiers

DOI
10.1088/0264-9381/26/9/094002;
PII
S0264-9381(09)98463-5;

Publishing Information

Journal Title
Classical and Quantum Gravity
Journal Volume
26
Journal Issue
9
Journal Page Range
[9 p.]
ISSN
0264-9381
CODEN
CQGRDG

Conference

Title
7. international LISA symposium
Dates
16-20 Jun 2008
Place
Barcelona (Spain)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
41105970
Subject category
S46: INSTRUMENTATION RELATED TO NUCLEAR SCIENCE AND TECHNOLOGY;
Resource subtype / Literary indicator
Conference
Descriptors DEI
ACTUATORS; COMPUTER CODES; CONTROL; DESIGN; ENGINEERING; GRAVITATIONAL WAVES; PROPULSION; PROPULSION SYSTEMS; SENSORS; SIMULATORS; SPACE FLIGHT
Descriptors DEC
ANALOG SYSTEMS; FUNCTIONAL MODELS