: Control Techniques for Responsive Space & Uncertain Systems Call 0017 — Air Force -- Research Lab funding opportunity
Air Force -- Research Lab · Federal agency

: Control Techniques for Responsive Space & Uncertain Systems Call 0017

BROAD AGENCY ANNOUNCEMENT BAA-VS-07-03Air Force Research Laboratory/Space Vehicles DirectoratePROPOSAL CALL ANNOUNCEMENT CALL 0017BROAD AGENCY ANNOUNCEMENT TITLE: Space Components Technology Open 5 Year Broad Agency Anno...

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Award $0–$1.5M Deadline 6385 days ago Location Alabama Type grant Level Federal Closed posted Feb 12, 2009
✦ AI Summary
  • Who can apply: Federal-level applicants (see eligibility for details).
  • Funding amount: up to $1,490,000.
  • Next deadline: February 23, 2009.
  • Issued by: Air Force -- Research Lab.
How was this generated?

The “key facts” mode pulls structured fields directly from the official source posting (amount, deadline, eligibility tags). The AI mode adds a short plain-English narrative on top, generated from the same source. Always verify with the agency before applying.

AI-generated. Always verify with the official source.

Who can apply — at a glance

  • Eligible applicants: see the Eligibility tab for the criteria from the official announcement.
  • Where: Alabama, Alaska, Arizona, Arkansas, California, Colorado, Connecticut, Delaware, Florida, Georgia, Hawaii, Idaho, Illinois, Indiana, Iowa, Kansas, Kentucky, Louisiana, Maine, Maryland, Massachusetts, Michigan, Minnesota, Mississippi, Missouri, Montana, Nebraska, Nevada, New Hampshire, New Jersey, New Mexico, New York, North Carolina, North Dakota, Ohio, Oklahoma, Oregon, Pennsylvania, Rhode Island, South Carolina, South Dakota, Tennessee, Texas, Utah, Vermont, Virginia, Washington, West Virginia, Wisconsin, Wyoming, District of Columbia.
  • Award: $0–$1.5M.
  • Matching funds: not required.
  • Deadline type: Fixed.

Compiled from the official listing's structured fields — always verify with the funder before applying.

About the funder

Air Force -- Research Lab is a federal-level funder.

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Award amount
$0–$1.5M
Deadline
6385 days ago
Feb 23, 2009

About this opportunity

BROAD AGENCY ANNOUNCEMENT BAA-VS-07-03Air Force Research Laboratory/Space Vehicles DirectoratePROPOSAL CALL ANNOUNCEMENT CALL 0017BROAD AGENCY ANNOUNCEMENT TITLE: Space Components Technology Open 5 Year Broad Agency Announcement.BROAD AGENCY ANNOUNCEMENT NUMBER: BAA-VS-07-03; Topic Area # 2 PROPOSAL CALL ANNOUCEMENT (CALL) TITLE: Control Techniques for Responsive Space & Uncertain SystemsPROPOSAL CALL ANNOUNCEMENT (CALL) NUMBER: 0017TECHNICAL POINT OF CONTACT: The technical point of contact for this CALL is Dr. Lawrence Robertson, AFRL/RVSV, Kirtland 505-846-7787, Fax 505-846-7787, Email Lawrence.Robertson@ CONTRACTING POINTS OF CONTACT: The contracting points of contact for this CALL are: Contract Specialist: Ms. Tara Bond, Det 8 AFRL/RVKV, Kirtland 505-846-4967, Fax 505-846-7041, Email [email protected], or Contracting Officer: Ms. Jeannie Barnes, Det 8 AFRL/RVKV, Kirtland 505-846-4695, Fax 505-846-7041, Email [email protected] DESCRIPTION: There are three basic need areas: (1) Adaptive Control Techniques for Responsive Launch Vehicle Ascent Guidance and Control, (2) Responsive Space Attitude Determination and Control – Reducing Guidance, Navigation and Control System Design and (3) Uncertainty Accommodating Control. These areas are described below. Note that an offeror may bid on all three areas. However, offerors must submit separate technical/cost proposals and should clearly delineate each specific area. 1. Adaptive Control Techniques for Responsive Launch Vehicle Ascent Guidance and Control. The Air Force’s needs for achieving operationally responsive access to space will require a responsive launch capability. Executing time-critical missions will require far greater capability of the guidance systems than currently exist for launch vehicles. The driving motivation for this research is that the challenges for realizing a responsive launch capability lie not only in hardware and operations, but also equally in software and algorithms. Traditionally, launch guidance and control (G&C) software and related parameters are designed for a specified launch mission (launch site, range constraints, etc.), payload, and targeting, or insertion, condition. This is a time-consuming process, done well in advance of the launch mission. Until the technical challenges associated with update and design of G&C algorithms and software on a short notice are satisfactorily addressed, on-demand responsive launch will not be possible even for a vehicle already on the launch pad. Application of both optimal control theories and adaptive control theories, combined with innovative numerical methods, will play a central role in advancing launch vehicle G&C technology necessary to meet the goals of responsive launch.The objectives of this effort are to:• Establish the degree of pre-mission planning and lead time required with the current launch vehicle ascent technology, and identify the portion attributable to G&C.• Identify candidate adaptive/optimal launch vehicle guidance and control algorithms and develop algorithm enhancements where appropriate.• Establish well defined evaluation criteria to assess candidate algorithms.• Develop testing scenarios and conduct simulations to demonstrate the benefits of adaptive/optimal closed-loop launch vehicle guidance and control technology.2. Responsive Space Attitude Determination and Control – Reducing Guidance, Navigation and Control System DesignThe Department of Defense is currently interested in reducing Guidance, Navigation and Control System Design and Integration Time for responsive space missions. The reduction of satellite design and integration time will allow for quicker replacement of failed satellites, improving communication and imaging capabilities. One of the primary concepts for achieving this is to reduce the amount of time available for ground-based calibration of satellite hardware and software.

Funding agency

Air Force -- Research Lab
Federal agency

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Citation details

Source systemgrants.gov
Source ID45101
PostedFeb 12, 2009

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