JWST Wavefront Sensing and Control

The precise optical alignment of the telescope optics for JWST is achieved and maintained using wavefront sensing imagery from the science instruments, particularly NIRCam, as well as actuators on the back of each mirror segment (including the secondary mirror).

Upon launch and deployment of the observatory, Optical Telescope Element (OTE) commissioning proceeded through several stages of iterative sensing and alignment correction over several months to establish the initial best on-orbit alignments. Once commissioned, the telescope is routinely monitored and corrections to maintain the mirror alignment are issued only occasionally. 

On this page

Active optics ops concept for JWST

Because of the unique circumstances of the stable space environment, the wavefront sensing system architecture on JWST is different from large active telescopes on the ground. Most significantly, JWST is free from atmospheric disturbances and gravity-induced deformations, which are the dominant factors requiring rapid correction for active and adaptive telescopes on Earth. Instead, JWST only needs corrections for wavefront aberrations that change much more slowly than the durations of typical science observations. In particular, the need for wavefront corrections during science operations is mostly due to temperature changes that cause slight thermal expansion and contraction of portions of the observatory, typically on timescales of several days. This allows the use of the science instrument imaging detectors for periodic measurements, rather than requiring dedicated wavefront sensor detectors or continuously active segment edge sensors.

NIRCam is the primary wavefront sensor for JWST and, because of its importance to overall observatory operations, comprises 2 fully redundant modules. Both NIRCam modules contain several components in its pupil and filter wheels that are used to measure the wavefront (e.g., weak lenses, Dispersed Hartmann sensors). In general, wavefront information is retrieved using focus-diverse phase retrieval, where the focus diversity is provided by the use of a combination of weak lenses (although during commissioning the multi-instrument/field diversity was provided by moving the secondary mirror). Analysis and determination of the wavefront error is performed on the ground using downlinked image data. The necessary mirror commands are then uplinked back to JWST to correct the alignments. Other instruments were used during OTE commissioning to assess the multi-field wavefront and optimize optical performance across the field of view.

Each primary mirror segment has actuators on its back that provide 6 degrees of freedom, as well as control over the radius of curvature. The secondary mirror is also controlled in its 6 degrees of freedom. Thus, there are a total of 132 degrees of freedom in the telescope that need alignment, plus the focus mechanisms in each of the science instruments apart from MIRI. Other alignments, such as the tertiary and fine steering mirror, were established during observatory assembly on the ground and are sufficiently rigid to not need correction in-flight.



Commissioning and initial alignment

After launch and deployment, the primary mirror segments, secondary, and science instruments were misaligned relative to each other by a small amount. An iterative process using several types of wavefront sensing and control was used to bring these mirrors into alignment within tens of nanometers. The large dynamic range (millimeters to nanometers) means that several distinct stages and types of sensing were necessary. This commissioning process was necessarily iterative, due to finite sensing precision and also to mechanism uncertainties inherent to the coarse stage actuator design. As a result, OTE commissioning was iterative at both small scales (a given step may need to be performed several times to converge) and at much larger scales (mechanism uncertainties required looping back to repeat entire sections of the commissioning plan).

The deployment of the secondary mirror, the two 3-mirror folded wing sections of the primary mirror, and initial deployments of segments from their launch restraints took place starting around 16 days after launch. The wavefront sensing and correction process began as soon as the telescope and instruments had cooled sufficiently close to their operating temperatures. This process interspersed individual wavefront sensing and control activities, initial activation and checkouts of the science instruments, and observatory-level calibration tasks that involve many subsystems across the whole observatory, such as the guider and attitude control system.

The main stages of OTE commissioning were (1) segment location and identification, (2) segment-level wavefront control, (3) segment co-phasing, and (4) multi-instrument (multi-field) sensing and control (see Figure 1 below). Because NIRCam is the main wavefront sensing sensor, high quality images were first achieved on NIRCam prior to any of the other instruments, around about halfway through telescope commissioning, then the multi-instrument sensing process adjusted the secondary mirror alignment to optimize image quality over the full instrument suite. The OTE commissioning lasted several months and was completed around mid-April 2022; it was followed by a thermal stability characterization assessment aimed at measuring the observatory's response to changes in spacecraft attitude with respect to the Sun.

Continued quantification of stability in flight will better inform ongoing wavefront maintenance. OTE commissioning was followed by the commissioning of the science instruments, during which period the OTE wavefront was routinely measured and corrected, as needed.

For more information on OTE commissioning, see Acton et al. (2012)Perrin et al. (2016), and, more recently, Acton et al. (2022).

Figure 1. Overview of the OTE Commissioning process

Click on the figure for a larger view.

Schematic of the overall OTE commissioning process, with representative flight data. The process was iterative and allowed for ultimately resulted in a telescope delivering better-than-expected optical performance in all of the science instruments. See Acton et al. (2022) for more details.


Routine wavefront sensing and control

See Optics Performance and Stability under JWST Observatory Characteristics and Performance for details of current optical stability and maintenance.



References

Acton, D. S., et al. 2022, SPIE 12180, 121800U
Phasing the Webb Telescope

Acton, D. S., et al. 2012, SPIE 8442, 84422H
Wavefront sensing and controls for the James Webb Space Telescope 

Perrin, M. D., et al. 2016, SPIE 9904, 99040F
Preparing for JWST wavefront sensing and control operations




Notable updates
  •  
    Article underwent major reorganization - content about science operations moved to Optics Performance and Stability

  •  
    Updated Figure 2, trending of the wavefront error in the science era

  •  
    Added updates based on commissioning data

  •   
    Reviewed and updated for Cycle 1 Call for Proposals release.
Originally published