Vehicle attitude control using movable mass

Patent metadata

Field	Value
Publication number	US-10414518-B2
Application number	US-201615344636-A
Country	US
Kind code	B2
Filing date	Nov 7, 2016
Priority date	Jul 2, 2014
Publication date	Sep 17, 2019
Grant date	Sep 17, 2019

Abstract

Attitude of a vehicle may be controlled using movable mass. The movable mass may move inside a vehicle or its outline, outside of the vehicle or its outline, inside-to-outside and/or outside-to-inside of the vehicle or its outline, or any combination thereof. The movable mass may be a solid, liquid, and/or gas. When the center-of-mass of the vehicle is moved relative to the line-of-action of applied forces such as thrust, drag, or lift, a torque can be generated for attitude control or for other purposes as a matter of design choice. In the case of external movable masses that extend from the vehicle or its outline, when operating in endoatmospheric flight, or general travel through a fluid, aerodynamic forces from the atmosphere or general fluid forces may further be leveraged to control the attitude of the vehicle (e.g., aerodynamic flaps).

First claim

The invention claimed is:

1. A vehicle attitude control system for controlling attitude and/or attitude rate of a vehicle subject to applied forces whose lines of action intersect within the vehicle or within an outline of the vehicle, comprising:
one or more movable masses configured to move a center-of-mass of the vehicle; and
a computing system configured to:
periodically or continuously calculate an attitude and attitude rate of the vehicle, and
when the attitude and/or attitude rate are not at desired values, perform an attitude and/or attitude rate correction by moving at least one of the one or more movable masses to achieve the desired values based on the calculated attitude and attitude rate to counteract a current angular acceleration and return the vehicle to a desired attitude and/or attitude rate, wherein

the one or more movable masses are external to the vehicle or the outline of the vehicle.

2. The vehicle attitude control system of claim 1 , wherein at least one of the one or more movable masses is internal to the vehicle or the outline of the vehicle.

3. A vehicle attitude control system for controlling attitude and/or attitude rate of a vehicle subject to applied forces whose lines of action intersect within the vehicle or within an outline of the vehicle, comprising:
one or more movable masses configured to move a center-of-mass of the vehicle; and a computing system configured to:
periodically or continuously calculate an attitude and attitude rate of the vehicle, and
when the attitude and/or attitude rate are not at desired values, perform an attitude and/or attitude rate correction by moving at least one of the one or more movable masses to achieve the desired values based on the calculated attitude and attitude rate to counteract a current angular acceleration and return the vehicle to a desired attitude and/or attitude rate of, wherein
at least one of the one or more movable masses is attached proximate to an exhaust nozzle of a rocket motor or engine; wherein the one or more movable masses are external to the vehicle or the outline of the vehicle.

4. A vehicle attitude control system for controlling attitude and/or attitude rate of a vehicle subject to applied forces whose lines of action intersect within the vehicle or within an outline of the vehicle, comprising:
one or more movable masses configured to move a center-of-mass of the vehicle; and
a computing system configured to:
periodically or continuously calculate an attitude and attitude rate of the vehicle, and
when the attitude and/or attitude rate are not at desired values, perform an attitude and/or attitude rate correction by moving at least one of the one or more movable masses to achieve the desired values based on the calculated attitude and attitude rate to counteract a current angular acceleration and return the vehicle to a desired attitude and/or attitude rate, wherein

at least one of the one or more movable masses extends partially or fully outward from the vehicle or the outline of the vehicle.

5. A vehicle attitude control system for controlling attitude and/or attitude rate of a vehicle subject to applied forces whose lines of action intersect within the vehicle or within an outline of the vehicle, comprising:
one or more movable masses configured to move a center-of-mass of the vehicle; and
a computing system configured to:
periodically or continuously calculate an attitude and attitude rate of the vehicle, and
when the attitude and/or attitude rate are not at desired values, perform an attitude and/or attitude rate correction by moving at least one of the one or more movable masses to achieve the desired values based on the calculated attitude and attitude rate to counteract a current angular acceleration and return the vehicle to a desired attitude and/or attitude rate, wherein

at least one movable mass is internal to the vehicle or the outline of the vehicle and at least one movable mass is partially or fully external to the vehicle or the outline of the vehicle.

6. A vehicle attitude control system for controlling attitude and/or attitude rate of a vehicle subject to applied forces whose lines of action intersect within the vehicle or within an outline of the vehicle, comprising:
one or more movable masses configured to move a center-of-mass of the vehicle; and
a computing system configured to:
periodically or continuously calculate an attitude and attitude rate of the vehicle, and
when the attitude and/or attitude rate are not at desired values, perform an attitude and/or attitude rate correction by moving at least one of the one or more movable masses to achieve the desired values based on the calculated attitude and attitude rate to counteract a current angular acceleration and return the vehicle to a desired attitude and/or attitude rate, wherein

at least one movable mass is configured to be moved from an inside of the vehicle or the outline of the vehicle to partially or fully outside of the vehicle or the outline of the vehicle, and vice versa, via an opening in an exterior or the outline of the vehicle.

7. The vehicle attitude control system of claim 1 , wherein when the vehicle is not rotating and is then subject to a thrust misalignment that causes the vehicle to begin rotating, the attitude and attitude rate correction comprises:
moving at least one of the one or more movable masses to cause an opposite angular acceleration to an initial angular acceleration such that rotation of the vehicle slows and stops, and the vehicle then begins to rotate back in an opposite direction,
moving at least one of the one or more movable masses to slow the rotation of the vehicle in the opposite direction such that the rotation in the opposite direction stops, and
moving at least one of the one or more movable masses such that a center of mass of the vehicle intersects a line of action of thrust of the vehicle.

8. The vehicle attitude control system of claim 3 , wherein when the vehicle is not rotating and is then subject to a thrust misalignment that causes the vehicle to begin rotating, the attitude and attitude rate correction comprises:
moving at least one of the one or more movable masses to cause an opposite angular acceleration to an initial angular acceleration such that rotation of the vehicle slows and stops, and the vehicle then begins to rotate back in an opposite direction,
moving at least one of the one or more movable masses to slow the rotation of the vehicle in the opposite direction such that the rotation in the opposite direction stops, and
moving at least one of the one or more movable masses such that a center of mass of the vehicle intersects a line of action of thrust of the vehicle.

9. The vehicle attitude control system of claim 4 , wherein when the vehicle is not rotating and is then subject to a thrust misalignment that causes the vehicle to begin rotating, the attitude and attitude rate correction comprises:
moving at least one of the one or more movable masses to cause an opposite angular acceleration to an initial angular acceleration such that rotation of the vehicle slows and stops, and the vehicle then begins to rotate back in an opposite direction,
moving at least one of the one or more movable masses to slow the rotation of the vehicle in the opposite direction such that the rotation in the opposite direction stops, and
moving at least one of the one or more movable masses such that a center of mass of the vehicle intersects a line of action of thrust of the vehicle.

10. The vehicle attitude control system of claim 5 , wherein when the vehicle is not rotating and is then subject to a thrust misalignment that causes the vehicle to begin rotating, th

Assignees

• Aerospace Corp

Inventors

• Zondervan Kevin L
• Fuller Jerome K

Classifications

• F42B10/60

  Steering arrangements (F42B19/01 takes precedence) · CPC title

• F02K9/90

  using deflectors (F02K9/82 takes precedence) · CPC title

• F02K9/80

  characterised by thrust or thrust vector control (burning control of solid propellants F02K9/26; feeding control of liquid or gaseous propellants F02K9/56; re-ignitable, restartable or intermittently operated rocket-engine plants F02K9/94) · CPC title

• F02K1/002

  with means to modify the direction of thrust vector (F02K1/54 takes precedence; thrust vectoring of rockets F02K9/80) · CPC title

• B64G1/28 Primary

  using inertia or gyro effect · CPC title