摘要:
Attitude acquisition methods and systems are provided which reduce the time generally required to acquire spacecraft attitude estimates and enhance the probability of realizing such estimates. The methods and systems receive, over a time span &Dgr;t, successive frames of star-sensor signals that correspond to successive stellar fields-of-view, estimate spacecraft rotation &Dgr;r throughout at least a portion of the time span &Dgr;t, and, in response to the spacecraft rotation &Dgr;r, process the star-sensor signals into a processed set of star-sensor signals that denote star positions across an expanded field-of-view that exceeds any of the successive fields-of-view. The expanded field-of-view facilitates identification of the stars that generated the processed set of star-sensor signals to thereby acquire an initial attitude estimate.
摘要:
A method of deriving a formula (FIG. 4) for calculating a quantity of fuel injected by an electric-actuated fuel injector (16) during an injection wherein duration of the injection is set by duration of an electric signal (P1, P2) applied to the fuel injector and pressure (ICP) at which the fuel is injected is set by pressure of hydraulic fluid applied to the fuel injector. The fuel injector is mapped by applying, various combinations of different selected hydraulic fluid pressures and different selected durations of the electric signal to create data sets of the corresponding selected hydraulic fluid pressure, the corresponding selected electric signal duration, and the quantity of fuel injected. Data from the data sets is processed to create terms of a multiple term mathematical formula that is used to calculate the quantity of fuel injected.
摘要:
In an engine capable of continuously controlling an intake air quantity by varying an intake valve operating characteristic, an intake valve lift is sensed as well as an engine speed. Then, an intake air quantity is calculated in accordance with the engine speed and intake valve lift when an engine operating point is in a very low lift state.
摘要:
A vehicle behavior control device includes a turning limit state detecting device for detecting a turning limit state of a vehicle and an engine output control device for performing a torque-down control by decreasing an engine output when the turning limit state of the vehicle is detected. The engine output control device includes a longitudinal acceleration detecting device, a lateral acceleration detecting device, a road friction coefficient estimating device, a maximum longitudinal acceleration calculating device for calculating a maximum longitudinal acceleration from the estimated road friction coefficient by the road friction coefficient estimating device and the lateral acceleration detected by the lateral acceleration estimating device, and a margin calculating device for calculating a margin of the longitudinal acceleration of the vehicle as a deviation between the maximum longitudinal acceleration calculated by the maximum longitudinal acceleration calculating device and the longitudinal acceleration detected by the longitudinal acceleration detecting device.
摘要:
A power window switch circuit, even if soaked, prevents windows from opening or closing unintentionally. A DOWN switch (128) and an UP switch (129) each include a first fixed contact (DN1, UP1) connected with a power supply, a second fixed contact (DN2, UP2) grounded, and movable contacts (131, 132, 133, 134) for selectively connects either the first or second fixed contact with the first terminal of corresponding relay coils (21, 23). A transistor (TR4) responsive to a soak signal is connected between the ground and the second fixed contacts (DN2, UP2) of the UP and DOWN switches. The second terminals of the first and second relay coils are grounded through their respective transistors. When a soak is detected, a soak detector (15) supplies a soak signal to the transistors.
摘要:
A classifying system 10 for a host vehicle 12 includes a sensor 14 and a controller 24 coupled to the host vehicle 12. The sensor 14 detects boundary data of an obstacle 16, 18, 20 and 22. The sensor 14 also generates an obstacle signal, which is received by the controller 24, which then generates a bounding box 26, 28, 30 and 32 for the obstacle 16, 18, 20 and 22. The bounding box 26, 28, 30 and 32 includes a number of vertical pixels 40, corresponding to a maximum height of the obstacle 16, 18, 20 and 22, and a number of horizontal pixels 42, corresponding to a maximum width of the obstacle 16, 18, 20 and 22. The controller 24 includes obstacle classifying logic activating in response to height and width of the obstacle 16, 18, 20 and 22 within parameters of one of a plurality of objects.
摘要:
A vehicle traveling control system is comprised of a following controller and a lane-keeping controller. The following controller controls an inter-vehicle distance between a host vehicle and a following object ahead of the host vehicle by controlling a vehicle speed on the basis of a detected inter-vehicle distance. The lane-keeping controller controls a steering control of the host vehicle so as to locate the host vehicle within a lane traveled by the host vehicle. A control condition of one of the following control and the steering control is changed according to the control condition of the other of the following control and the steering control.
摘要:
A flight control system for controlling a flight of an aircraft, having an actuator for actuating flight control surfaces and outputting a feedback signal in return; a flight control computer for operating the actuator; and an actuator control computer for controlling the operation of the actuator. The flight control computer comprises an FCC processor for generating an instruction signal to operate the actuator on the basis of an operational instruction signal inputted from a pilot and a state signal indicative of the state of an aircraft, and generating a reference signal on the basis of the instruction signal and the feedback signal from the actuator. The actuator control computer comprises an ACC processor for generating an actuator control signal on the basis of the instruction signal generated by the FCC processor and the feedback signal from the actuator, and a servo amplifier for amplifying the actuator control signal generated by the ACC processor to be outputted to the actuator. The actuator is operative to actuate the flight control surfaces in accordance with the actuator control signal amplified by the servo amplifier and output a feedback signal in return. The flight control computer further comprises a comparing section for comparing the actuator control signal generated by the ACC processor with the reference signal generated by the FCC processor to detect a failure wherein the FCC processor is different in design from the ACC processor.
摘要:
A method and system for automatically activating a train warning device that uses a positioning system such as a global positioning system (GPS) receiver or an inertial navigation system (INS) to determine the train's position. The system further includes a database containing locations of grade crossings and other locations at which a train is required to give a warning signal and what regulations govern activation of the warning device at such locations.