Impact discriminating apparatus for missiles and the like, and method for impact discrimination

Claim 2

In combination with a movable object having impact responsive function performing means, impact discriminating means for controlling said function performing means, which comprises: a. a plurality of impact sensors disposed within said object in spaced relationship generally along a predetermined line of Impact, said sensors having electrical output signals responsive to impact shocks received by said sensors, and b. electronic comparing means cooperating with said sensors and said function performing means for comparing said sensor output signals and for causing operation of said function performing means only when said sensor output signals indicate occurrence of an impact in a predetermined direction along said predetermined line of impact.

Claim 3

The invention as claimed in claim 1, wherein said comparing means includes pulse height discrimination means for rejecting said sensor output signals which are below a predetermined level, whereby effects of impacts below a predetermined impact level are blanked out.

Claim 4

The invention as claimed in claim 1, wherein said comparing means includes pulse generating means associated with each of said sensors for separately receiving said output signals therefrom, and for causing pulse generator output pulses having predetermined pulse widths associated with each of said sensors.

Claim 5

The invention as claimed in claim 3, wherein said pulse generating means includes blanking means for blanking out effects of subsequent output signals received from said sensors which occur within a predetermined time after first output signals are received therefrom, whereby effects of shock waves rearwardly reflected from said impact region along said predetermined line of impact are blanked out.

Claim 6

The invention as claimed in claim 3, wherein each of said sensors has associated therewith a different pulse generator pulse width, said pulse width varying according to the position of said sensors along said predetermined line of impact, said pulse width associated with sensors close to a predetermined impact region being longer than said pulse widths associated with sensors more remote from said impact region, said pulse widths being sufficient to cause overlapping of pulses from a preselected number of said pulse generating means when a shock wave is propagated in said predetermined direction along said predetermined line of impact, and being insufficient to cause overlapping of pulses from said preselected number of said pulse generating means when a shock wave is propagated in a direction opposite to said predetermined direction.

Claim 7

The invention as claimed in claim 5, wherein said comparing means includes gating means having inputs connected to said pulse generating means and having an output connected to said function performing means, the output of said gating means being initially in a first state and being caused to change to a second state to operate said function performing means when, and only when, said overlapping pulses from said preselected number of said pulse generating means are received by said inputs.

Claim 8

In a missile having fusing or detonating means, impact discriminating means for operating said fusing or detonating means, which comprises: a. a plurality of impact sensors arranged in spaced relationship along a predetermined line of impact and comparatively adjacent to a predetermined impacting point, said sensors having electrical output signals responsive to impact shocks received by said sensors, b. pulse generating means electrically connected to said sensors for receiving electrical signals from said sensors in response to impact shock waves sensed thereby, said pulse generating means including pulse generators associated with each of said sensors, for converting electrical outputs therefrom into generator output pulses having predetermined pulse widths varying with the position of an associated sensor along said line of impact, said predetermined pulse widths decreasing with increasing distances of said associated sensors from said impacting point and being such that a shock wave propagating rearwardly from said impacting point through said missile and along said predetermined line of impact causes overlapping of said pulses, but a shock wave propagated forwardly through said missile, along said predetermined line of impact towards said impacting point does not cause overlapping of said pulses, and c. gating means for causing operation of said fusing or detonating means, said gating means having inputs into which are directed said generator output pulses, and having an output initially in a first state not causing operating of said fusing or detonating means, said output being caused to change to a second state operating said fusing or detonating means only when generator output pulses received from each of said pulse generators are in an overlapping relationship, whereby operation of said fusing and detonating means is caused by a shock wave propagating rearwardly through said missile along said predetermined line of impact from said impacting point, but not by a shock wave traveling in the opposite direction.

Claim 9

In a missile having fusing or detonating means, impact discriminating means for operating said fusing or detonating means, which comprises: a. a plurality of impact sensors arranged in spaced relationship along a predetermined line of impact and comparatively adjacent to a predetermined impacting point, said sensors having electrical output signals responsive to impact shocks received by said sensors, b. pulse generating means electrically connected to said sensors for receiving electrical signals from said sensors in response to impact shock waves sensed thereby, said pulse generating means including pulse generators associated with each of said sensors, for converting electrical outputs therefrom into generator output pulses having predetermined pulse widths varying with the position of an associated sensor along said line of impact, said predetermined pulse widths decreasing with increasing distances of said associated sensors from said impacting point and being such that a shock wave propagating rearwardly from said impacting point through said missile and along said predetermined line of impact causes overlapping of said pulses, but a shock wave propagated forwardly through said missile, along said predetermined line of impact towards said impacting point does not cause overlapping of said pulses, and c. gating means for causing operation of said fusing or detonating means, said gating means having inputs into which are directed said generator output pulses, and having an output initially in a first state not causing operating of said fusing or detonating means, said output being caused to change to a second state operating said fusing or detonating means only when generator output pulses received from each of said pulse generators are in an overlapping relationship, whereby operation of said fusing and detonating means is caused by a shock wave propagating rearwardly through said missile along said predetermined line of impact from said impacting point, but not by a shock wave traveling in the opposite direction.

Claim 10

The invention as claimed in claim 7, including blanking means for causing disregarding of second output signals from said sensors received within a predetermined time after first output signals are received therefrom, whereby effects of shock waves rearwardly reflected from said impact point, and caused by shock waves traveling forwardly along said predetermined line of impact, are disregarded.

Claim 11

The invention as claimed in claim 7, including pulse height discriminating means for causing said sensor electrical outputs associated with impact shocks below a predetermined level to be disregarded, regardless of direction of propagation of the resulting shock waves, whereby said fusing or detonating means may be operated only by impact shocks above said predetermined shock level.

Claim 14

The method as claimed in claim 10, including the step of blanking out effects of second electrical output signals received from said sensors within a predetermined time after first output signals are received therefrom, whereby effects of reflected shock waves are disregarded.

Claim 15

The method as claimed in claim 10, including the step of disregarding electrical output signals from said sensors which have a magnitude below a predetermined level, whereby the effects of impact shock below a predetermined level are disregarded, regardless of the direction of propagation of the resulting impact shock wave.

Claim 16

The method as claimed in claim 10, including the step of operating a function performing means only when said overlapping pulses are received by said discriminating element.