US4164018A — Method and apparatus for steering a spacecraft an…

Claim 1

Independent Claim 119 words

An inertial device for regulating the on-board voltage of a spacecraft and for steering said spacecraft comprising at least two contra-rotating dynamo-electric machines with alternating magnetic fields and having motor and generator modes of operation, solar generator means to power said machines, power switching means connected to said machines to connect said solar generator means to said machines during said motor mode of said machines, velocity control means also connected to said machines during said motor mode, said power switching means also connected to said machines to connect an on-board electrical load of the spacecraft to said machines during said generator mode of said machines, and control means for determining the time of opening of said power switching means.

Claim 2

Dependent Claim 119 words

An inertial device for regulating the on-board voltage of a spacecraft and for steering said spacecraft comprising at least two contra-rotating dynamo-electric machines with alternating magnetic fields and having motor and generator modes of operation, solar generator means to power said machines, power switching means connected to said machines to connect said solar generator means to said machines during said motor mode of said machines, velocity control means also connected to said machines during said motor mode, said power switching means also connected to said machines to connect an on-board electrical load of the spacecraft to said machines during said generator mode of said machines, and control means for determining the time of opening of said power switching means.

Claim 3

Dependent Claim 249 words

The inertial device as claimed in claim 1 wherein each of said dynamo-electric machines includes a rotor supported in magnetic bearings and having at least six rotating field magnets each formed by a permanent magnet with said magnets being spaced a magnetic half-pitch apart and said alternating magnetic fields being radial, and a stator having at least four coils in the form of turns set at a magnetic pitch and having at least one strand opposite said permanent magnets, said turns being spaced one-half magnetic pitch apart, with said strands of said turns intercepting said magnetic fields to produce upon switching of said coils, in said motor mode, a torque given by the relation φ=BIlN.sup.b R[1-(n/N).sup.2 ] where: B is the magnetic induction intercepting said strands, I is the mean current flowing in each of said turns, φ is the active length of a strand, N b is the number of said strands, R is the positioning radius of said strands, n/N is the ratio of the number of commanded advance positions to the total number of possible positions; and in said generator mode, an electromotive force E, determined by the relations: ##EQU13## where: n/N is the ratio of the number of commanded opening positions to the total possible number of positions, ω o is the nominal angular velocity of the generator, ω is the true angular velocity of the generator, and E o is the no-load electromotive force of the machine at the angular velocity ω o .

Claim 4

Dependent Claim 77 words

The inertial device as claimed in claim 1 wherein said control means includes two sensors each comprising an oscillator means whose self-inductance is constituted by a ring fastened with a stator of each of said machines, metallic segments fastened with a rotor of each of said machines passing through an air gap of said rings to modify the quality factor thereof, the voltage produced being filtered and applied to a comparator which provides a logic control signal.

Claim 5

Dependent Claim 42 words

The inertial device as claimed in claim 3 wherein each metallic segment has a length of one magnetic pitch, said segments being spaced from one another by one magnetic pitch, and said rings are spaced from each other by one magnetic half-pitch.

Claim 6

Dependent Claim 114 words

The inertial device as claimed in claim 1 wherein said power switching means includes power switches each comprising firstly, high voltage transistors cascade-connected to pass the total current passing through each said switch also through each of the coils of said machine it controls, and, secondly, associated diodes which eliminate all reverse voltage at the terminals of said switch, each of said switches being controlled from voltage generators which generate a 60 V supply for application when said machines operate in said generator mode, and a 5 V supply applied during operation of said machines in said motor mode, and a supply of determinate voltage for speeding up said machines during an acquisition phase.

Claim 7

Dependent Claim 82 words

The inertial device as claimed in claim 1 wherein interconnection switches, diodes and blocking diodes are connected to said solar generator means and to the on-board electrical load of the spacecraft, said interconnection switches being conducting during operation of said machines in said generator mode, and said blocking diodes isolating said solar generator means during operation of said machines in said generator mode and isolating one of said machines from the other in the event of breakdown of one of said machines.

Claim 8

Independent Claim 294 words

A method of regulating the onboard voltage of a spacecraft and of steering said spacecraft by an inertial device having at least two contra-rotating dynamo-electric machines operating during periods of illumination as motors powered by solar generators through power switches, and during periods of occultation as generators connected to an on-board electric load through said power switches, said method comprising the steps of: in the motor mode of the machines, applying switching control signals on the power switches to adjust the switching to take place in advance with respect to the nominal opening time of said switches in order to change the rotational speed of the machines; in the generator mode of the machines, applying switching control signals on the power switches to adjust the switching duration of said switches to maintain the on-board voltage constant notwithstanding variations in speed; said control signals applied so as to affect the machines in such manner that, without a steering correction, when the speeds of the machines are equal, said speeds follow a pre-established theoretical law of speed, when the speeds of the machines are different, said speeds vary while maintaining the speed difference imposed by the last steering correction produced by the steering device of the spacecraft, after said speed difference had previously been memorized, upon the appearance of a steering correction order, said speeds of the machines vary both as a function of the pre-established theoretical law of speed and of the instantaneous speed difference imposed by the steering device; and further including obtaining the instantaneous speed difference by integrating an error signal provided by the steering device; and controlling the pre-established theoretical law of speed by a clock having its frequency slaved to the on-board voltage when the machines operate in the generator mode.

Claim 9

Independent Claim 294 words

A method of regulating the onboard voltage of a spacecraft and of steering said spacecraft by an inertial device having at least two contra-rotating dynamo-electric machines operating during periods of illumination as motors powered by solar generators through power switches, and during periods of occultation as generators connected to an on-board electric load through said power switches, said method comprising the steps of: in the motor mode of the machines, applying switching control signals on the power switches to adjust the switching to take place in advance with respect to the nominal opening time of said switches in order to change the rotational speed of the machines; in the generator mode of the machines, applying switching control signals on the power switches to adjust the switching duration of said switches to maintain the on-board voltage constant notwithstanding variations in speed; said control signals applied so as to affect the machines in such manner that, without a steering correction, when the speeds of the machines are equal, said speeds follow a pre-established theoretical law of speed, when the speeds of the machines are different, said speeds vary while maintaining the speed difference imposed by the last steering correction produced by the steering device of the spacecraft, after said speed difference had previously been memorized, upon the appearance of a steering correction order, said speeds of the machines vary both as a function of the pre-established theoretical law of speed and of the instantaneous speed difference imposed by the steering device; and further including obtaining the instantaneous speed difference by integrating an error signal provided by the steering device; and controlling the pre-established theoretical law of speed by a clock having its frequency slaved to the on-board voltage when the machines operate in the generator mode.

Annuity Stage	Window Opens	Payment Deadline	Surcharge Period Until	Estimated Fee	Status
3.5 Years (Year 4)	1982-08-06	1983-02-05	1983-08-07	$2000.00	Window Closed / Lapsed
7.5 Years (Year 8)	1986-08-06	1987-02-05	1987-08-07	$3760.00	Window Closed / Lapsed
11.5 Years (Year 12)	1990-08-06	1991-02-05	1991-08-07	$7700.00	Window Closed / Lapsed

Method and apparatus for steering a spacecraft and regulating its onboard supply voltage

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