Acceleration error compensated attitude sensing and control apparatus and method

An error compensated attitude sensing apparatus comprising a framework,

• an angular accelerometer mounted on said framework providing an angular acceleration indicative output,
• a tilt sensor mounted in said framework providing an angle of tilt indicative output, said angle of tilt being relative to a reference plane,
• said tilt sensor having a tilt axis and a linear acceleration sensing axis in orthogonal relation, said tilt axis being aligned substantially parallel with said angular acceleration sensing axis,
• means for receiving and converting said angular acceleration indicative output to an angle indicative output,
• means for receiving said angle indicative output and said angle of tilt indicative output and providing a combined angle indicative output,
• said last named output being connected to the input of said means for receiving and converting so that transients and drift in said angle indicative output are compensated,
• said framework having a center of rotation and said tilt sensor being mounted a predetermined distance therefrom,
• means for connecting a predetermined portion of said angular acceleration indicative output to said angle of tilt indicative output, said predetermined portion being dependent upon said predetermined distance,
• whereby signal components in said angle of tilt indicative output due to tangential acceleration of said tilt sensor are compensated.

An error compensated attitude sensing apparatus comprising a supporting structure,

• an angular accelerometer mounted on said supporting structure for providing an angular acceleration indicative output, said angular accelerometer having an acceleration sensing axis and a cross axis orthogonal thereto which is linear acceleration sensitive, whereby in the presence of linear acceleration said angular acceleration indicative output includes a cross axis sensitivity output component,
• a tilt sensor mounted on said support structure providing an angle of tilt indicative output which is relative to a reference plane,
• said tilt sensor having a tilt axis and a linear acceleration sensing axis oriented orthogonal thereto,
• said tilt axis being aligned substantially parallel with said angular acceleration sensing axis and said cross axis being aligned substantially parallel with said linear acceleration sensing axis,
• and means for coupling said angle of tilt indicative output to said angular acceleration indicative output in predetermined proportion to substantially cancel said cross axis sensitivity component.

An error compensated attitude sensing apparatus comprising a support structure,

• a tilt sensor mounted on said support structure providing an angle of tilt indicative output referenced to a predetermined plane, said tilt sensor having a tilt axis, and a linear acceleration sensing axis oriented orthogonally thereto,
• an angular accelerometer mounted on said support structure providing an angular acceleration indicative output, said angular accelerometer having an angular acceleration sensing axis and a linear acceleration sensitive axis oriented orthogonally thereto, so that in the presence of linear acceleration said angular acceleration indicative output contains a linear acceleration sensitive component, said tilt axis being aligned substantially parallel to said angular acceleration sensing axis and said linear acceleration sensitive axis being aligned substantially parallel to said angular accelerometer linear acceleration sensitive axis,
• means for receiving and converting said angular acceleration indicative output to an angle indicative output, means for coupling said angle of tilt indicative output to said angle indicative output, said angle of tilt indicative output having a scale factor similar to said angle indicative output whereby a combined angle indicative output is provided, said means for receiving and converting having fast response relative to said means for coupling said angle of tilt indicative output, whereby transient outputs in said angle of tilt indicative output are substantially eliminated from said combined angle indicative output, said support structure having a center of rotation and said tilt sensor being mounted a predetermined distance therefrom, together with means for coupling a predetermined portion of said angular acccleration indicative output to said angle of tilt indicative output, said predetermined portion being related to said predetermined distance, so that error signal produced by tangential acceleration sensed by said tilt sensor and appearing in said angle of tilt indicative output is substantially cancelled.

An error compensated attitude sensing apparatus comprising a support structure,

• a tilt sensor mounted on said support structure providing an angle of tilt indicative output referenced to a predetermined plane, said tilt sensor having a tilt axis, and a linear acceleration sensing axis oriented orthogonally thereto,
• an angular accelerometer mounted on said support structure providing an angular acceleration indicative output, said angular accelerometer having an angular acceleration sensing axis and a linear acceleration sensitive axis oriented orthogonally thereto, so that in the presence of linear acceleration said angular acceleration indicative output contains a linear acceleration sensitive component, said tilt axis being aligned substantially parallel to said angular acceleration sensing axis and said linear acceleration sensitive axis being aligned substantially parallel to said angular accelerometer linear acceleration sensitive axis,
• means for receiving and converting said angular acceleration indicative output to an angle indicative output, means for coupling said angle of tilt indicative output to said angle indicative output, said angle of tilt indicative output having a scale factor similar to said angle indicative output whereby a combined angle indicative output is provided, said means for receiving and converting having fast response relative to said means for coupling said angle of tilt indicative output,
• whereby transient outputs in said angle of tilt indicative output are substantially eliminated from said combined angle indicative output, said support structure including a platform together with a framework, means for supporting said support structure in said framework for rotational motion therewith,
• and an additional angular accelerometer mounted on said framework providing an additional angular acceleration indicative output related to the angular acceleration thereof,
• said framework having a center of rotation with said tilt sensor mounted a predetermined distance therefrom,
• means for coupling a predetermined portion of said additional angular acceleration indicative output to said angle of tilt indicative output, said predetermined portion depending on said predetermined distance, so that components in said angle indicative output due to tangential acceleration of said tilt sensor are substantially removed.

An error compensated attitude sensing apparatus comprising a support structure,

• an angular accelerometer mounted on said support structure providing an angular acceleration indicative output, said angular accelerometer having an angular acceleration sensing axis and a linear acceleration sensitive axis oriented orthogonal thereto, said angular acceleration indicative output thereby having a linear acceleration sensitive output component included in the presence of linear acceleration,
• a tilt sensor mounted on said support structure providing an angle of tilt indicative output related to a reference plane,
• said tilt sensor having a tilt axis and a linear acceleration sensitive axis is orthogonal relation, said tilt axis being aligned substantially parallel with said angular acceleration sensing axis and said linear acceleration sensing axis being aligned substantially parallel with said angular accelerometer linear acceleration sensitive axis,
• means for coupling a predetermined portion of said angle of tilt indicative output to said angular acceleration indicative output so that said linear acceleration sensitivity output component is substantially cancelled,
• means for passing low frequency angle of tilt indicative output,
• means for passing high frequency angular acceleration indicative output,
• means for combining said high and low frequency outputs providing an angle output,
• a platform mounted on said support structure for rotational movement therewith about at least one axis,
• means mounted on said one axis for urging said platform rotationally toward a rotational position responsive to said angle output.

An error compensated acceleration sensor for mounting on a body to be acceleration monitored, the body having an axis of rotation, comprising

• an angular accelerometer mounted on the body providing an angular acceleration output, said angular accelerometer having an angular acceleration sensing axis,
• a linear accelerometer mounted on the body providing a linear acceleration sensitive output and having a linear acceleration sensitive axis, said linear accelerometer being mounted a predetermined distance from the axis or rotation,
• whereby said linear acceleration indicative output contains a component corresponding to tangential acceleration of said linear accelerometer when the body is accelerated about the axis of rotation,
• and means for coupling a signal portion of said angular acceleration indicative output to said linear acceleration indicative output, said signal portion being determined by said predetermined distance and the ratio of linear acceleration indicative output scale factor to angular acceleration indicative output scale factor, whereby error in said linear acceleration indicative output due to tangential acceleration of the body is reduced.

An error compensated attitude sensing apparatus comprising

• a support structure havng a center of rotation
• an angular accelerometer mounted on said support structure for producing an angular acceleration indicative output,
• a tilt sensor mounted on said support structure a predetermined distance from said center of rotation for producing an angle of tilt indicative output wherein said angle of tilt is relative to a reference plane,
• said tilt sensor having a tilt axis and a linear acceleration sensing axis in orthogonal relation, said tilt axis being aligned substantially parallel with said angular acceleration sensing axis and said linear acceleration sensing axis having a component aligned along the direction between said tilt sensor and said center of rotation, whereby said angle of tilt indicative output contains a component corresponding to radial acceleration when said support structure is moving at an angular velocity about said center of rotation,
• means for receiving said angular acceleration indicative output and for producing an angular velocity indicative output and an angle indicative output,
• means for receiving said angle indicative output and said angle of tilt indicative output and producing a combined angle indicative output,
• and means for coupling a signal portion of said angular velocity indicative output to said tilt indicative output, said signal portion being determined by said predetermined distacne and the square of said angular velocity indicative output, whereby error in said tilt indicative output due to radial acceleration of said support structure is reduced.