Engineering of the LISA Pathfinder mission-making the experiment a practical reality
Creators
- 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/10.1088/0264-9381/26/9/094002Additional 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