Abstract
The MAXIM (Mico-Arcsecond X-Ray Imaging Mission) and MAXIM Pathfinder, a technology precursor mission, is considered by NASA as "visionary missions" in space astronomy. Currently the MAXIM mission design would fly multiple spacecraft in formation, each carrying precision optics, to direct X-rays from an astronomical source to collector and imaging spacecrafts. The mission architecture is complex and provides technical challenges in formation flying and external metrology, spacecraft pointing control, active internal spacecraft metrology, and target acquisition. To further develop the concept, an integrated model (IM) of the MAXIM and MAXIM Pathfinder was developed. Individual subsystem models from disciplines in structural dynamics, optics, controls, signal processing, detector physics and disturbance modeling are seamlessly integrated into one cohesive model to efficiently support system level trades and analysis. The optical system design is a unique combination of optical concepts and therefore results from the IM were extensively compared with ASAP optical software.
| Original language | English |
|---|---|
| Pages (from-to) | 557-567 |
| Number of pages | 11 |
| Journal | Proceedings of SPIE - The International Society for Optical Engineering |
| Volume | 4851 |
| Issue number | 1 |
| DOIs | |
| State | Published - 2002 |
| Event | X-ray and Gamma-Ray telescopes and Instruments for Astronomy - Waikoloa, HI, United States Duration: Aug 24 2002 → Aug 28 2002 |
Keywords
- Diffraction
- End-to-end modeling
- Integrated modeling
- MATLAB
- MAXIM
- Ray tracing
- Simulink
- X-ray optics