Hybrid power unmanned aerial vehicle energy source control method based on power following
A hybrid, energy control technology, applied in aircraft power units, aircraft parts, transport hydrogen technology, etc., can solve the problems of shortened service life, large weather effects, and high power density
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Embodiment 1
[0093] Implementation example 1: take off at 6:00 on the winter solstice day
[0094] Step 1, establish the UAV flight environment model, set the initial conditions of the UAV flight and the state parameters of the hybrid UAV energy system (including solar cells, lithium batteries and fuel cells).
[0095] 1.1 The initial state of the UAV: the take-off time is 6:00 in the morning of the winter solstice, the location is 40 degrees north latitude, 116 degrees east longitude, heading due east, press image 3 The flight profile of the UAV, the take-off weight of the UAV is 15kg, and it starts from rest at 3m / s 2 Accelerate to 12m / s to take off the ground, climb to 500m at a constant speed with a 4° climb angle, and turn to level flight, and accelerate to 15m / s with a maximum lift-to-drag ratio of 18 and continue cruising for 3 hours before gliding and landing without power.
[0096] 1.2 Energy system parameters: the lower limit parameter of the available power of solar cells is...
Embodiment 2
[0110] Implementation example 2: take off at 11:00 on the winter solstice day
[0111] Step 1, the takeoff time is 11:00 on the winter solstice day, other initial value settings are the same as step 1 in (1);
[0112] Step 2 is the same as step 2 in (1);
[0113] Step 3, step up =2, update step=3, monitor the current maximum output power of the solar cell such as Figure 4 (b) as shown in P arrary =136.6W>P available =10W, the solar battery is available, update the current step step=3.2, and execute step 5;
[0114] Step 5, step up =3.2, update step=5, calculate the remaining power P of the solar cell:
[0115] P=P arrary -P d =136.6-15.0=121.6W>0
[0116] Execute step 4, the result is SOC=1>SOC high For case 4.2, the excess power P of the solar battery is used for the climbing of the UAV, and the electric energy is converted into gravitational potential energy storage. The hybrid UAV energy system controls three power outputs as follows:
[0117] ...
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