Kinematics with Constant Acceleration and MEMS Accelerometers

Miniature MEMS Accelerometers

  • Micro-Electro-Mechanical Systems (MEMS) accelerometers are integrated-circuit devices smaller than a single millimeter.

  • Structural Components:

    • A thin cantilever anchored to the substrate acts as a mechanical spring.
    • A tiny metallic moveable block is attached to the cantilever.
    • A stationary electrode is positioned adjacent to the moveable block, forming a capacitor.
  • Working Mechanism:

    • Acceleration along the axis of motion causes the moveable block to sway toward or away from the fixed electrode.
    • The displacement scale of the moveable block is approximately 0.5mm0.5\,\text{mm}.
    • The physical displacement alters the capacitive distance, modifying an electric current flowing through a circuit connected to a voltage source and current meter.
    • Continuous monitoring of this electrical current allows precise real-time inference of acceleration along the acceleration axis.
  • Multi-Axis Sensing and Kinematics:

    • Most commercial devices integrate three independent orthogonal sensors to measure acceleration across all three spatial dimensions simultaneously.
    • Numerical integration of a continuous acceleration record yields real-time changes in velocity and position.
  • Practical Applications:

    • Used in navigation systems, robotics, medical devices, and wearable fitness trackers.

Schematic diagram and physical microchip layout of a miniature accelerometer

Derivation of One-Dimensional Constant-Acceleration Kinematic Equations

  • Position relative to Velocity-Time Integration:

    • The final position sfs_{\text{f}} along a spatial coordinate axis ss is equal to the initial position sis_{\text{i}} added to the total area bounded by the velocity curve vsv_s between initial time tit_{\text{i}} and final time tft_{\text{f}}:     sf=si+area under velocity curve vs between ti and tfs_{\text{f}} = s_{\text{i}} + \text{area under velocity curve } v_s \text{ between } t_{\text{i}} \text{ and } t_{\text{f}}
  • Derivation of Position-Time Kinematic Equation:

    • Under constant acceleration asa_s, the velocity graph is a straight line starting at initial velocity visv_{\text{is}}.
    • The area under the velocity line over elapsed time Δt=tfti\Delta t = t_{\text{f}} - t_{\text{i}} forms a trapezoid divisible into two distinct geometric regions:
    • A rectangular area representing initial displacement:       Arearectangle=visΔt\text{Area}_{\text{rectangle}} = v_{\text{is}} \, \Delta t
    • A triangular area representing displacement accumulated due to acceleration:       Areatriangle=12(asΔt)(Δt)=12as(Δt)2\text{Area}_{\text{triangle}} = \frac{1}{2} (a_s \, \Delta t)(\Delta t) = \frac{1}{2} a_s (\Delta t)^2
    • Summing these component areas yields the second core kinematic equation:     sf=si+visΔt+12as(Δt)2s_{\text{f}} = s_{\text{i}} + v_{\text{is}} \, \Delta t + \frac{1}{2} a_s (\Delta t)^2
    • The quadratic dependence on elapsed time Δt\Delta t causes the position-versus-time graph for constant acceleration to form a parabola.
  • Derivation of Time-Independent Kinematic Equation:

    • Velocity under constant acceleration is given by:     vfs=vis+asΔtv_{\text{fs}} = v_{\text{is}} + a_s \, \Delta t
    • Rearranging to express elapsed time Δt\Delta t in terms of velocity and acceleration:     Δt=vfsvisas\Delta t = \frac{v_{\text{fs}} - v_{\text{is}}}{a_s}
    • Substituting this expression into the position equation yields:     sf=si+vis(vfsvisas)+12as(vfsvisas)2s_{\text{f}} = s_{\text{i}} + v_{\text{is}} \left( \frac{v_{\text{fs}} - v_{\text{is}}}{a_s} \right) + \frac{1}{2} a_s \left( \frac{v_{\text{fs}} - v_{\text{is}}}{a_s} \right)^2
    • Algebraic expansion and rearrangement gives the third basic kinematic equation:     vfs2=vis2+2asΔsv_{\text{fs}}^2 = v_{\text{is}}^2 + 2 a_s \, \Delta s
    • The quantity Δs=sfsi\Delta s = s_{\text{f}} - s_{\text{i}} represents spatial displacement (net change in position, distinct from total path distance).

The Constant-Acceleration Model

  • Model Principles and Assumptions:

    • Few physical objects experience perfectly uniform acceleration; however, approximating motion as constant acceleration provides an accurate predictive framework while avoiding unnecessary mathematical complexity.
    • Objects such as sprinters, automobiles, airplanes, and rockets are commonly modeled with constant acceleration.
    • A physical model consists of defined assumptions, pictorial representations, graphs, and mathematical equations.
  • Graphical Behavior in the Constant-Acceleration Model:

    • Acceleration vs. Time (asa_s vs tt): Represented by a horizontal straight line (as=constanta_s = \text{constant}).
    • Velocity vs. Time (vsv_s vs tt): Represented by a straight line with y-intercept visv_{\text{is}} and constant slope equal to acceleration asa_s
    • Position vs. Time (ss vs tt): Represented by a parabola with initial position sis_{\text{i}}, where the instantaneous slope at any point equals velocity vsv_s

Model 2.2 Constant Acceleration Motion Diagrams and Graphs

  • Summary of Core Mathematical Equations:

    • vfs=vis+asΔtv_{\text{fs}} = v_{\text{is}} + a_s \, \Delta t
    • sf=si+visΔt+12as(Δt)2s_{\text{f}} = s_{\text{i}} + v_{\text{is}} \, \Delta t + \frac{1}{2} a_s (\Delta t)^2
    • vfs2=vis2+2asΔsv_{\text{fs}}^2 = v_{\text{is}}^2 + 2 a_s \, \Delta s
  • Model Limitation:

    • The model fails if the object's acceleration varies over the interval of motion.

Kinematic Problem-Solving Strategy

  • MODEL:

    • Model the moving object as a point particle undergoing constant acceleration.
  • VISUALIZE:

    • Draw a clear pictorial representation establishing coordinate axes and defining discrete physical points of interest.
    • Translate physical motion statements into mathematical variables and constants.
    • Construct motion graphs (acceleration, velocity, position versus time) as appropriate.
  • SOLVE:

    • Apply the primary kinematic equations:     vfs=vis+asΔtv_{\text{fs}} = v_{\text{is}} + a_s \, \Delta tsf=si+visΔt+12as(Δt)2s_{\text{f}} = s_{\text{i}} + v_{\text{is}} \, \Delta t + \frac{1}{2} a_s (\Delta t)^2vfs2=vis2+2asΔsv_{\text{fs}}^2 = v_{\text{is}}^2 + 2 a_s \, \Delta s
    • Replace generic symbol ss with axis-specific position variables (xx or yy).
    • Replace generic initial/final subscripts (i\text{i}, f\text{f}) with numerical indices (0,1,2,0, 1, 2, \dots) established in the pictorial representation.
  • REVIEW:

    • Verify that units and significant figures are correct, that the result is physically reasonable, and that the exact question asked has been answered.

Step-by-Step Kinematics Example: Motion of a Rocket Sled

  • Problem Context:

    • A rocket sled's engines fire for 5.0s5.0\,\text{s}, accelerating the sled to a velocity of 250m/s250\,\text{m/s}.
    • A braking parachute deploys, decelerating the sled at a rate of 3.0m/s3.0\,\text{m/s} per second (3.0m/s23.0\,\text{m/s}^2) until it comes to a complete stop.
    • Objective: Determine the total distance traveled by the sled.
  • Modeling Phase:

    • The sled is aerodynamic, making air resistance minimal; model as a particle undergoing two consecutive constant-acceleration stages (boost stage and braking stage).
  • Visualization and Subscript Assignment:

    • Point 0 (Start of boost): x0=0mx_0 = 0\,\text{m}, v0x=0m/sv_{0x} = 0\,\text{m/s}, t0=0st_0 = 0\,\text{s}
    • Point 1 (Engine burnout / parachute deployment): x1x_1, v1x=250m/sv_{1x} = 250\,\text{m/s}, t1=5.0st_1 = 5.0\,\text{s}
    • Point 2 (Complete stop): x2x_2, v2x=0m/sv_{2x} = 0\,\text{m/s}, t2t_2
    • Interval Accelerations:
    • a0xa_{0x}: Acceleration during propulsion phase (interval 0 to 1).
    • a1x=3.0m/s2a_{1x} = -3.0\,\text{m/s}^2: Leftward acceleration during braking phase (interval 1 to 2).

Pictorial representation of the rocket sled motion showing three stages: start, deploy parachute, and stop

  • Mathematical Solution:

    • Phase 1: Boost Phase Analysis (Interval 0 to 1):

    • Determine boost acceleration a0xa_{0x} using velocity-time equation:       v1x=v0x+a0x(t1t0)=a0xt1v_{1x} = v_{0x} + a_{0x}(t_1 - t_0) = a_{0x} t_1

    • Solve algebraically for a0xa_{0x}:       a0x=v1xt1=250m/s5.0s=50m/s2a_{0x} = \frac{v_{1x}}{t_1} = \frac{250\,\text{m/s}}{5.0\,\text{s}} = 50\,\text{m/s}^2

    • Calculate distance traveled during boost x1x_1 using position-time equation:       x1=x0+v0x(t1t0)+12a0x(t1t0)2=12a0xt12x_1 = x_0 + v_{0x}(t_1 - t_0) + \frac{1}{2} a_{0x}(t_1 - t_0)^2 = \frac{1}{2} a_{0x} t_1^2x1=12(50m/s2)(5.0s)2=625mx_1 = \frac{1}{2} (50\,\text{m/s}^2)(5.0\,\text{s})^2 = 625\,\text{m}

    • Phase 2: Braking Phase Analysis (Interval 1 to 2):

    • Apply time-independent kinematic equation over displacement Δx=x2x1\Delta x = x_2 - x_1:       v2x2=v1x2+2a1xΔx=v1x2+2a1x(x2x1)v_{2x}^2 = v_{1x}^2 + 2 a_{1x} \, \Delta x = v_{1x}^2 + 2 a_{1x}(x_2 - x_1)

    • Rearrange algebraically to solve for final position x2x_2:       x2=x1+v2x2v1x22a1xx_2 = x_1 + \frac{v_{2x}^2 - v_{1x}^2}{2 a_{1x}}

    • Substitute numerical values:       x2=625m+0(250m/s)22(3.0m/s2)x_2 = 625\,\text{m} + \frac{0 - (250\,\text{m/s})^2}{2(-3.0\,\text{m/s}^2)}x2=625m+62,500m2/s26.0m/s2=625m+10,416.67m=11,041.67mx_2 = 625\,\text{m} + \frac{-62,500\,\text{m}^2/\text{s}^2}{-6.0\,\text{m}/\text{s}^2} = 625\,\text{m} + 10,416.67\,\text{m} = 11,041.67\,\text{m}

    • Round to two significant figures:       x2=11,000mx_2 = 11,000\,\text{m}

  • Execution Insights:

    • Perform algebraic manipulation completely prior to inserting numerical values to prevent intermediate calculation errors.
    • Maintain extra significant figures in intermediate distances (x1=625mx_1 = 625\,\text{m}) to preserve precision prior to final rounding.