Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
240 words
In a pendulous induction compass transmitter compensated for errors due to the Earth's vertical field during turns, the combination comprising: a. magnetic sensing means for producing modulated signals proportional to the strength of the Earth's field along the fore/aft and athwartships axes of an aircraft; b. means to demodulate the modulated signal representative of the sensed fore/aft field to produce a varying, DC, demodulated signal proportional to the sensed Earth's field along the fore/aft axis of the aircraft and thus to the cosine of the magnetic heading angle ψ and of the aircraft; c. means to demodulate the modulated signal representative of the sensed athwartships field to produce a varying, DC, demodulated signal proportional to the sensed Earth's field along the athwartships axis of the aircraft and thus to the sine of the magnetic heading angle ψ of the aircraft; d. means to compensate the demodulated signals for errors due to the Earth's vertical field during turns, including; 1. means to generate a DC correction signal proportional to the product of the Earth's magnetic field M, the sine of the magnetic dip angle D and the sine of the bank angle φ, 2. means to add said DC correcting signal algebraically to said demodulated DC signal proportional to the Earth's field and thus to the sine of the magnetic heading angle ψ to cancel the signal component due to the Earth's vertical field sensed along the athwartships axis during turns.
Claim 2
Dependent Claim
240 words
In a pendulous induction compass transmitter compensated for errors due to the Earth's vertical field during turns, the combination comprising: a. magnetic sensing means for producing modulated signals proportional to the strength of the Earth's field along the fore/aft and athwartships axes of an aircraft; b. means to demodulate the modulated signal representative of the sensed fore/aft field to produce a varying, DC, demodulated signal proportional to the sensed Earth's field along the fore/aft axis of the aircraft and thus to the cosine of the magnetic heading angle ψ and of the aircraft; c. means to demodulate the modulated signal representative of the sensed athwartships field to produce a varying, DC, demodulated signal proportional to the sensed Earth's field along the athwartships axis of the aircraft and thus to the sine of the magnetic heading angle ψ of the aircraft; d. means to compensate the demodulated signals for errors due to the Earth's vertical field during turns, including; 1. means to generate a DC correction signal proportional to the product of the Earth's magnetic field M, the sine of the magnetic dip angle D and the sine of the bank angle φ, 2. means to add said DC correcting signal algebraically to said demodulated DC signal proportional to the Earth's field and thus to the sine of the magnetic heading angle ψ to cancel the signal component due to the Earth's vertical field sensed along the athwartships axis during turns.
Claim 3
Dependent Claim
69 words
The pendulous induction compass transmitter according to claim 1 wherein said magnetic sensing means produces three phase output signals representative of the sensed field along the respective axes and includes means for converting the three phase output signals from said magnetic sensing means to a pair of signals representative of the product of the Earth's magnetic field and the sine and cosine of the magnetic heading angle ψ respectively.
Claim 4
Dependent Claim
47 words
The pendulous induction compass transmitter according to claim 2 wherein said means for converting includes a Scott-Tee transformer having a three phase input to which the three phase signals from the magnetic sensing means are coupled and a two phase output coupled to the said demodulating means.
Claim 5
Dependent Claim
119 words
The pendulous induction compass transmitter according to claim 1 including further means to compensate for two cycle error comprising a. first and second closed loop, null balanced modulating means each having an input and an output and the compensated demodulated DC signals coupled thereto, each of said modulating means including a negative feedback path from its output to its input, b. demodulating means in each of said negative feedback paths, c. means to reduce the negative feedback in one of said paths by a factor proportional to the cosine of the bank angle φ whereby the output signal of the modulator associated with the said one negative feedback path is increased correspondingly to cancel two cycle error during turns.
Claim 6
Dependent Claim
70 words
The pendulous induction compass transmitter according to claim 4 wherein said means to reduce the negative feedback in said one path includes; 1. multiplying means in said path and, 2. means to apply the output signal from the associated modulating means and a signal proportional to the cosine of the bank angle φ during a turn to said multiplier to reduce the feedback by the cosine of bank angle φ.