Velocity and drift angle tracking system using altimetry signals

• US 4,103,302 A
• Filed: 07/16/1976
• Issued: 07/25/1978
• Est. Priority Date: 07/16/1976
• Status: Expired due to Term

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: General Electric Company
• Inventors: Roeder, Allan W., Kimball, Richard M., Koschmeder, Richard F.
• Primary Examiner(s): Wilbur, Maynard R.
• Assistant Examiner(s): Goodwin, Lawrence
• Application Number:
  US05/705,881
• Time in Patent Office: 739 Days
• Field of Search: 343/8, 343/9 R, 343/100 SA, 343/100 CL, 343/7.5, 340/3 R
• US Class Current: 342/113
• CPC Class Codes: G01S 13/605 using a pattern, backscattered from the ground, to determine speed or drift by measuring the time required to cover a fixed distance

Abstract

A system for determining the magnitude and direction of the relative velocity of two objects wherein a first of the objects, for example an aircraft, transmits a continuous sequence of radar pulses from a broad beam antenna directed toward the second object, e.g., the ground, and a receiver, also mounted on the aircraft, receives the echo returns of the pulses through an antenna which has a pair of phase center locations spaced apart along the axis of the aircraft. The two receiving phase centers are electrically displaceable in directions lateral to the aircraft axis (heading) and are controlled to follow substantially the same ground track. The positions of the phase centers are also "dithered" laterally to enable automatic tracking of aircraft drift angle. Reflected pulses received at the forward and aft phase center locations are non-coherently detected and a computing system performs a time-amplitude comparison of the pulse amplitude values detected at the aft phase center location against the pulse amplitude values detected at the forward phase center location N pulse repetition intervals earlier in time. The relative velocity between the aircraft and the ground is calculated as a function of the pulse repetition frequency.

Claims

1. A system for determining the drift angle of a fluid-born vehicle, said drift angle being defined as the angle between the vehicle heading direction and the direction said vehicle is moving relative to an adjacent stationary reflecting surface, said system comprising, in combination:

transmitting means provided on said vehicle for illuminating said surface with a train of wave energy pulses;

receiving means on said vehicle for receiving said wave energy after reflection from said surface, said receiving means having forward and aft energy-receiving phase centers spaced apart from one another in said vehicle heading direction;

offset means for electronically intermittantly shifting said forward and aft phase centers by selected amounts in directions lateral to said heading direction;

correlating means responsive to reflected wave energy pulses received at said forward and aft phase centers for processing selected pairs of said forward and aft received pulses to generate a crosscorrelation output indicative of the crosscorrelation of a plurality of said selected pairs, said correlating means further operating to generate a crosscorrelation difference output indicative of the difference between crosscorrelation outputs generated for different lateral positions of said phase centers and to generate an offset control signal in response to said crosscorrelation difference output, and wherein said correlating means includes means for sampling the amplitude of each of said received pulses and for storing an amplitude value F for each said forward pulse and an amplitude value A for each said aft pulse; and

crosscorrelation output means for generating said crosscorrelation outputs in accordance with the algorithm ##EQU6## where E {FA} represents the expected value of the products of said amplitude values for a predetermined number of said selected pairs of pulses;

η

_F η

_A represents the product of the mean values for the F and A values, respectively, in said predetermined number of selected pairs of pulses and σ

_F σ

_A represents the product of the standard deviation values for the F and A values, respectively, in said predetermined number of selected pairs of pulses;

electronic control means responsive to said offset control signal for controlling said offset means to alter the amount of lateral displacement of said phase centers so as to minimize said crosscorrelation difference output; and

calculating means responsive to the amount of said phase center displacement for generating a representation of drift angle.

2. The system set forth in claim 1 wherein each said selected pair of forward and aft pulses comprises a different aft-received pulse together with the forward-received pulse which was received N pulse repetition intervals earlier in time.

3. A system for determining the drift angle of a fluid-born vehicle, said drift angle being defined as the angle between the vehicle heading direction and the direction said vehicle is moving relative to an adjacent stationary reflecting surface, said system comprising, in combination:

transmiting means provided on said vehicle for illuminating said surface with a train of wave energy pulses;

receiving means on said vehicle for receiving said wave energy after reflection from said surface, said receiving means having forward and aft energy-receiving phase centers spaced apart from one another in said vehicle heading direction;

offset means for electronically intermittantly shifting said forward and aft phase centers by selected amounts in directions lateral to said heading direction;

correlating means responsive to reflected wave energy pulses received at said forward and aft pulse centers for processing selected pairs of said forward and aft received pulses to generate a crosscorrelation output indicative of the crosscorrelation of a plurality of said selected pairs, said correlating means further operating to generate a crosscorrelation difference output indicative of the difference between crosscorrelation outputs generated for different lateral positions of said phase centers and to generate an offset control signal in response to said crosscorrelation difference outputs;

electronic control means responsive to said offset control signal for controlling said offset means to alter the amount of lateral displacement of said phase centers so as to minimize said crosscorrelation difference output;

calculating means responsive to the amount of said phase center displacement for generating a representation of drift angle;

wherein said correlating means further includes means for generating a correlation output e_vi in accordance with the algorithm

space="preserve" listing-type="equation">e.sub.vi = 1/2[A.sub.N+i - F.sub.i)F.sub.i-2 - F.sub.i+2)+(A.sub.N+i+2 - F.sub.i+2) (F.sub.i - F.sub.i+4)]

where A_N+i and A_N+i+2 represent two consecutively received aft pulses, F_i and F_i+2 represent the forward pulses received immediately before and after said F_i pulse and F_i and F_i+4 represent the forward pulses received immediately before and after said F_i+2 pulse, the subscript i denoting a progression of alternate odd integers to indicate the chronological occurrence of said pulses and the subscript N denoting that each aft pulse of said pair is received N pulse repetition intervals later in time than its associated forward pulse;

means responsive to said correlation output for controlling said transmitting means to adjust the repetition frequency of said train of wave energy pulses such that said correlation output is maintained at a minimum value; and

means for determining said heading velocity based on the quotient of said phase center separation distance and N multiplied by the duration of the interval between pulses in said transmitted pulse train, and wherein said calculating means includes means responsive to said representations of heading velocity and drift angle for generating a representation of the drift velocity of said vehicle.

4. A system for determining the drift angle of an aircraft relative to the ground, said drift angle being defined as the angle between the vehicle heading direction and the direction said vehicle is moving relative to an adjacent stationary reflecting surface, said system compromising, in combination:

transmitting means provided on said aircraft for illuminating said surface with a train of rf pulses;

receiving means on said aircraft for receiving said rf pulses after reflection from said surface, said receiving means having forward and aft energy-receiving phase centers spaced apart from one another in said vehicle heading direction, wherein said receiving means further comprises a pair of forward antennas spaced apart from one another in said lateral direction;

a pair of aft antennas spaced apart from one another in said lateral direction; and

hybrid waveguide means for combining the rf energy received at said respective pairs of antennas such that said forward phase center is located on a phase center line joining the phase centers of said pair of forward antennas and said aft phase center is located on a phase center line joining the phase centers of said aft antennas;

offset means for electronically intermittantly shifting said forward and aft phase centers by selected amounts in directions lateral to said heading direction;

correlating means responsive to reflected rf pulses received at said forward and aft phase centers for processing selected pairs of said forward and aft received pulses to generate a crosscorrelation output indicative of the crosscorrelation of a plurality of said selected pairs, said correlating means further operating to generate a crosscorrelation difference output indicative of the difference between crosscorrelation outputs generated for different lateral positions of said phase centers and to generate an offset control signal in response to said crosscorrelation difference output;

electronic control means responsive to said offset control signal for controlling said offset means to alter the amount of lateral displacement of said phase centers so as to minimize said crosscorrelation difference output; and

calculating means responsive to the amount of said phase center displacement for calculating said drift angle.

5. The system set forth in claim 4 wherein said hybrid waveguide means comprises:

a first hybrid having input ports connected to receive the signals from said forward pair of antennas and having sum and difference output ports;

a second hybrid having input ports connected to receive the signals from said aft pair of antennas and having sum and difference output ports;

a third hybrid having a pair of input ports and a sum and difference output port;

means for alternately coupling the input ports of said third hybrid to the output ports of said first and second hybrids; and

variable signal attenuation means provided at one of the inputs to said third hybrid whereupon control of said attenuation means causes the signals presented at the output ports of said third hybrid to emanate from selected phase centers located on either of said forward of aft phase center lines.

6. The system set forth in claim 5 further comprising:

polarity selection means coupled to said third hybrid output ports and having an output line, said selection means being operable to couple one or the other of said third hybrid output ports to said output line whereby the signal on said output line is controlled to emanate from a single phase center on either said forward or said aft phase center line.

7. The system set forth in claim 5 wherein said offset means comprises:

means for generating an attenuation control signal;

means for coupling said control signal to said variable attenuation means to cause the signals produced at said third hybrid output ports to emanate from selected locations on said phase center lines; and

means for periodically changing said control signal to effect said intermittant shifting of said phase center locations between predetermined locations on said phase center locations between predetermined locations on said phase center lines.

8. The system set forth in claim 6 wherein said offset means comprises:

means for generating a polarity selection control signal;

means for coupling said attenuation and polarity selection control signals to said variable attentuation means and said polarity selection means, respectively, to cause the signal presented on said output line to emanate from a single predetermined location on each of said phase center lines; and

means for periodically changing said control signals to effect said intermittant shifting of said phase center locations between multiple predetermined locations on said phase center lines.