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Spacecraft Observatory Benchmark Problem for Optical Disturbance RejectionSince mid-1980s NASA has launched several first-generation interplanetary observatory missions. A salient feature of these missions has been the mounting of the optical payload on top of a large flexible space structure. This imposes challenging control-structure interaction problems (CSI) that have been studied over several decades. The Dec. 2021 launch of the James Webb Telescope marks the latest example of such a mission. One way to encourage development of novel control methods is to provide a benchmark problem for researchers. By the mid-2000s, there were a few well-known benchmark problems developed by the control community with a focus on CSI applications. However, in the past 15 years, the control challenges in optical observation missions have shifted from CSI to line-of-sight (LOS) precision pointing. This is because popular designs of the second-generation (Gen II) space earth missions have eliminated the large structure interface by mounting the optical payload directly on top of a rigid bus platform. The focus now is to achieve accurate pointing with maximum rejection of the surrounding disturbances. The NASA Safety and Engineering Center (NESC) has tasked T he Aerospace Corporation to develop a Benchmark Problem to study the challenging control issues that Gen II observatory missions encounter. This software tool is to be released as a public domain platform aimed at government, academic, and industry researchers. The focus of this benchmark problem is for researchers to design a set of innovative payload control laws with the maximum Optical Disturbance Rejection (ODR) capability to meet a set of pre-defined μrad-level of LOS jitter requirements. This paper describes the development of the benchmark problem. Aerospace/NASA will provide an integrated LOS plant model and disturbance/command profiles for users to run their design and simulation with as well as a user’s guide describing the required interfaces. The Aerospace Corp is also working to develop a hardware fast steering mirror testbed for users to demonstrate their innovative design in real hardware, if so desired.
Document ID
20220019350
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Cornelius Dennehy
(Langley Research Center Hampton, Virginia, United States)
Richard Y Chiang
(The Aerospace Corporation El Segundo, California, United States)
Richard M Dolphus
(The Aerospace Corporation El Segundo, California, United States)
Michael Andonian
(The Aerospace Corporation El Segundo, California, United States)
Wei Huang
(The Aerospace Corporation El Segundo, California, United States)
Thomas A Battista
(The Aerospace Corporation El Segundo, California, United States)
Uday J Shankar
(Johns Hopkins University Applied Physics Laboratory North Laurel, Maryland, United States)
Date Acquired
January 4, 2023
Subject Category
Optics
Meeting Information
Meeting: 45th Annual AAS Guidance, Navigation and Control Conference
Location: Breckenridge, CO
Country: US
Start Date: February 3, 2023
End Date: February 8, 2023
Sponsors: American Astronautical Society
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
Spacecraft Observatory Benchmark Problem
Optical Disturbance Rejection
Interplanetary Observatory Missions
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